Fwxm       !"#$%&'()*+,-./0123456789:;<=>?@ABCDEFGHIJKLMNOPQRSTUVWXYZ[\]^_`abcdefghijklmnopqrstuvwxyz{|}~      !"#$%&'()*+,-./0123456789:;<=>?@ABCDEFGHIJKLMNOPQRSTUVWXYZ[\]^_`abcdefghijklmnopqrstuvwxyz{|}~      !"#$%&'()*+,-./0123456789:;<=>?@ABCDEFGHIJKLMNOPQRSTUVWXYZ[\]^_`abcdefghijklmnopqrstuvwxyz{|}~      !"#$%&'()*+,-./0123456789:;<=>?@ABCDEFGHIJKLMNOPQRSTUVWXYZ[\]^_`abcdefghijklmnopqrstuvwxyz{|}~                                                                            ! " # $ % & ' ( ) * + , - . / 0 1 2 3 4 5 6 7 8 9 : ; < = > ? @ A B C D E F G H I J K L M N O P Q R S T U V W X Y Z [ \ ] ^ _ ` a b c d e f g h i j k l m n o p q r s t u v w x y z { | } ~                                                                                                                                                                   ! " # $ % & ' ( ) * + , - . / 0 1 2 3 4 5 6 7 8 9 : ; < = > ? @ A B C D E F G H I J K L M N O P Q R S T U V W X Y Z [ \ ] ^ _ ` a b c d e f g h i j k l m n o p q r s t u v w x y z { | } ~                                                           !"#$%&'()*+,-./0123456789:;<=>?@ABCDEFGHIJKLMNOPQRSTUVWXYZ[\]^_`abcdefghijklmnopqrstuvwxyz{|}~      !"#$%&'()*+,-./0123456789:;<=>?@ABCDEFGHIJKLMNOPQRSTUVWXYZ[\]^_`abcdefghijklmnopqrstuvwxyz{|}~      !"#$%&'()*+,-./0123456789:;<=>?@ABCDEFGHIJKLMNOPQRSTUVWXYZ[\]^_`abcdefghijklmnopqrstuvwxyz{|}~                                  ! " # $ % & ' ( ) * + , - . / 0 1 2 3 4 5 6 7 8 9 : ; < = > ? @ A B C D E F G H I J K L M N O P Q R S T U V W X Y Z [ \ ] ^ _ ` a b c d e f g h i j k l m n o p q r s t u v w x y z { | } ~                                                                                                                                                                   ! " # $ % & ' ( ) * + , - . / 0 1 2 3 4 5 6 7 8 9 : ; < = > ? @ A B C D E F G H I J K L M N O P Q R S T U V W X Y Z [ \ ] ^ _ ` a b c d e f g h i j k l m n o p q r s t u v w x y z { | } ~                                                                                                                                                                   ! " # $ % & ' ( ) * + , - . / 0 1 2 3 4 5 6 7 8 9 : ; < = > ? @ A B C D E F G H I J K L M N O P Q R S T U V W X Y Z [ \ ] ^ _ ` a b c d e f g h i j k l m n o p q r s t u v w x y z { | } ~                                                                                                                                                                   ! " # $ % & ' ( ) * + , - . / 0 1 2 3 4 5 6 7 8 9 : ; < = > ? @ A B C D E F G H I J K L M N O P Q R S T U V W X Y Z [ \ ] ^ _ ` a b c d e f g h i j k l m n o p q r s t u v w x y z { | } ~                                                                                                                                                                   ! " # $ % & ' ( ) * + , - . / 0 1 2 3 4 5 6 7 8 9 : ; < = > ? @ A B C D E F G H I J K L M N O P Q R S T U V W X Y Z [ \ ] ^ _ ` a b c d e f g h i j k l m n o p q r s t u v w x y z { | } ~                )Copyright (C) 2015 Swift Navigation, Inc.LGPL-3Mark Fine <dev@swiftnav.com> experimentalportableNone9Calculate CCITT 16-bit Cyclical Redundancy Check (CRC16).)Copyright (C) 2015 Swift Navigation, Inc.LGPL-3Mark Fine <dev@swiftnav.com> experimentalportableNone"# <Packet structure for Swift Navigation Binary Protocol (SBP).GDefinition of the over-the-wire message framing format and packet structure for Swift Navigation Binary Protocol (SBP), a minimal binary protocol for communicating with Swift devices. It is used to transmit solutions, observations, status and debugging messages, as well as receive messages from the host operating system.4Uniquely identifies the type of the payload contentsyA unique identifier of the sending hardware. For v1.0, set to the 2 least significant bytes of the device serial number Byte-length of the payload fieldBinary data of the message, as identified by Message Type and Length. Usually contains the in-memory binary representation of a C struct (see documentation on individual message types)Cyclic Redundancy Check (CRC) of the packet's binary data from the Message Type up to the end of Payload (does not include the Preamble)CWrapper around ByteString for *JSON and Binary typeclass instances. ?Denotes the start of frame transmission. For v1.0, always 0x55. KDefault sender ID. Intended for messages sent from the host to the device.UClass of generic representation of specialized SBP messages into SBP message frames.rConvert an SBP message record that is serializable and a two-byte senderID to a binary into an SBP message frame.   "!  )Copyright (C) 2015 Swift Navigation, Inc.LGPL-3Mark Fine <dev@swiftnav.com> experimentalportableNone0 ]Derive ToSBP typeclass, given an SBP message type name and the name of the implemented type. ;Derive JSON stripping out prefixes of the implemented type. .Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"##4SBP class for message MSG_BASELINE_HEADING (0x020F)."This message reports the baseline heading pointing from the base station to the rover relative to True North. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow). It is intended that time-matched RTK mode is used when the base station is moving.%GPS Time of Week&Heading'%Number of satellites used in solution( Status flags1/SBP class for message MSG_ORIENT_QUAT (0x0220).This message reports the quaternion vector describing the vehicle body frame's orientation with respect to a local-level NED frame. The components of the vector should sum to a unit vector assuming that the LSB of each component as a value of 2^-31.3GPS Time of Week4Real component51st imaginary component62nd imaginary component73rd imaginary component8!Estimated standard deviation of w9!Estimated standard deviation of x:!Estimated standard deviation of y;!Estimated standard deviation of z< Status flagsI0SBP class for message MSG_ORIENT_EULER (0x0221).This message reports the yaw, pitch, and roll angles of the vehicle body frame. The rotations should applied intrinsically in the order yaw, pitch, and roll in order to rotate the from a frame aligned with the local-level NED frame to the vehicle body frame.KGPS Time of WeekL.rotation about the forward axis of the vehicleM0rotation about the rightward axis of the vehicleN/rotation about the downward axis of the vehicleO$Estimated standard deviation of rollP%Estimated standard deviation of pitchQ#Estimated standard deviation of yawR Status flagse0SBP class for message MSG_ANGULAR_RATE (0x0222).This message reports the orientation rates in the vehicle body frame. The values represent the measurements a strapped down gyroscope would make and are not equivalent to the time derivative of the Euler angles. The orientation and origin of the user frame is specified via device settings. By convention, the vehicle x-axis is expected to be aligned with the forward direction, while the vehicle y-axis is expected to be aligned with the right direction, and the vehicle z-axis should be aligned with the down direction.gGPS Time of Weekhangular rate about x axisiangular rate about y axisjangular rate about z axisk Status flagsB#$%&'()123456789:;<=>?@AIJKLMNOPQRSTUVWXYZ[\]efghijklmnopqrst|}~R)#$%&'(*.//@?>=A123456789:;<BFGG\[ZYXWVUTS]IJKLMNOPQR^bccsrqponmltefghijkuyzz~}|#$%&'(1 23456789:;<I JKLMNOPQRefghijk.Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#C +SBP class for message MSG_STARTUP (0xFF00).The system start-up message is sent once on system start-up. It notifies the host or other attached devices that the system has started and is now ready to respond to commands or configuration requests.Cause of startup Startup typeReserved0SBP class for message MSG_DGNSS_STATUS (0xFF02).This message provides information about the receipt of Differential corrections. It is expected to be sent with each receipt of a complete corrections packet. Status flagsLatency of observation receipt#Number of signals from base stationCorrections source string-SBP class for message MSG_HEARTBEAT (0xFFFF).The heartbeat message is sent periodically to inform the host or other attached devices that the system is running. It is used to monitor system malfunctions. It also contains status flags that indicate to the host the status of the system and whether it is operating correctly. Currently, the expected heartbeat interval is 1 sec. The system error flag is used to indicate that an error has occurred in the system. To determine the source of the error, the remaining error flags should be inspected. Status flags.SBP class for message MSG_INS_STATUS (0xFF03).rThe INS status message describes the state of the operation and initialization of the inertial navigation system. Status flags..Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalTportable Messages for reading, writing, and discovering device settings. SettingsNone"#U1SBP class for message MSG_SETTINGS_SAVE (0x00A1).xThe save settings message persists the device's current settings configuration to its onboard flash memory file system.2SBP class for message MSG_SETTINGS_WRITE (0x00A0).The setting message writes the device configuration for a particular setting via A NULL-terminated and NULL-delimited string with contents !SECTION_SETTING\0SETTING\0VALUE\0 where the '\0' escape sequence denotes the NULL character and where quotation marks are omitted. A device will only process to this message when it is received from sender ID 0x42. An example string that could be sent to a device is "solution0soln_freq0100".;A NULL-terminated and NULL-delimited string with contents !SECTION_SETTING\0SETTING\0VALUE\07SBP class for message MSG_SETTINGS_WRITE_RESP (0x00AF).Return the status of a write request with the new value of the setting. If the requested value is rejected, the current value will be returned. The string field is a NULL-terminated and NULL-delimited string with contents !SECTION_SETTING\0SETTING\0VALUE\0 where the '\0' escape sequence denotes the NULL character and where quotation marks are omitted. An example string that could be sent from device is "solution0soln_freq0100". Write status6A NULL-terminated and delimited string with contents !SECTION_SETTING\0SETTING\0VALUE\05SBP class for message MSG_SETTINGS_READ_REQ (0x00A4).The setting message that reads the device configuration. The string field is a NULL-terminated and NULL-delimited string with contents SECTION_SETTING\0SETTING\0 where the '\0'D escape sequence denotes the NULL character and where quotation marks are omitted. An example string that could be sent to a device is "solution0soln_freq0". A device will only respond to this message when it is received from sender ID 0x42. A device should respond with a MSG_SETTINGS_READ_RESP message (msg_id 0x00A5).;A NULL-terminated and NULL-delimited string with contents SECTION_SETTING\0SETTING\06SBP class for message MSG_SETTINGS_READ_RESP (0x00A5).The setting message wich which the device responds after a MSG_SETTING_READ_REQ is sent to device. The string field is a NULL- terminated and NULL-delimited string with contents !SECTION_SETTING\0SETTING\0VALUE\0 where the '\0' escape sequence denotes the NULL character and where quotation marks are omitted. An example string that could be sent from device is "solution0soln_freq0100".;A NULL-terminated and NULL-delimited string with contents !SECTION_SETTING\0SETTING\0VALUE\0>SBP class for message MSG_SETTINGS_READ_BY_INDEX_REQ (0x00A2).oThe settings message for iterating through the settings values. A device will respond to this message with a MSG_SETTINGS_READ_BY_INDEX_RESP.RAn index into the device settings, with values ranging from 0 to length(settings)?SBP class for message MSG_SETTINGS_READ_BY_INDEX_RESP (0x00A7).The settings message that reports the value of a setting at an index. In the string field, it reports NULL-terminated and delimited string with contents .SECTION_SETTING\0SETTING\0VALUE\0FORMAT_TYPE\0 . where the '\0' escape sequence denotes the NULL character and where quotation marks are omitted. The FORMAT_TYPE field is optional and denotes possible string values of the setting as a hint to the user. If included, the format type portion of the string has the format "enum:value1,value2,value3". An example string that could be sent from the device is "simulator0enabled0True0enum:True,False0"RAn index into the device settings, with values ranging from 0 to length(settings)6A NULL-terminated and delimited string with contents .SECTION_SETTING\0SETTING\0VALUE\0FORMAT_TYPE\0?SBP class for message MSG_SETTINGS_READ_BY_INDEX_DONE (0x00A6).?The settings message for indicating end of the settings values.5SBP class for message MSG_SETTINGS_REGISTER (0x00AE).This message registers the presence and default value of a setting with a settings daemon. The host should reply with MSG_SETTINGS_WRITE for this setting to set the initial value.6A NULL-terminated and delimited string with contents SECTION_SETTING\0SETTING\0VALUE.-&Q   #$$& .Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#J%',SBP class for message MSG_GPS_TIME (0x0102).This message reports the GPS time, representing the time since the GPS epoch began on midnight January 6, 1980 UTC. GPS time counts the weeks and seconds of the week. The weeks begin at the Saturday/Sunday transition. GPS week 0 began at the beginning of the GPS time scale. Within each week number, the GPS time of the week is between between 0 and 604800 seconds (=60*60*24*7). Note that GPS time does not accumulate leap seconds, and as of now, has a small offset from UTC. In a message stream, this message precedes a set of other navigation messages referenced to the same time (but lacking the ns field) and indicates a more precise time of these messages.)GPS week number*3GPS time of week rounded to the nearest millisecond+ONanosecond residual of millisecond-rounded TOW (ranges from -500000 to 500000),Status flags (reserved)5,SBP class for message MSG_UTC_TIME (0x0103).This message reports the Universal Coordinated Time (UTC). Note the flags which indicate the source of the UTC offset value and source of the time fix.7"Indicates source and time validity83GPS time of week rounded to the nearest millisecond9Year:Month (range 1 .. 12);days in the month (range 1-31)<hours of day (range 0-23)=minutes of hour (range 0-59)>+seconds of minute (range 0-60) rounded down?)nanoseconds of second (range 0-999999999)L(SBP class for message MSG_DOPS (0x0208).This dilution of precision (DOP) message describes the effect of navigation satellite geometry on positional measurement precision. The flags field indicated whether the DOP reported corresponds to differential or SPP solution.NGPS Time of WeekOGeometric Dilution of PrecisionPPosition Dilution of PrecisionQTime Dilution of PrecisionR Horizontal Dilution of PrecisionSVertical Dilution of PrecisionTGIndicates the position solution with which the DOPS message correspondsf,SBP class for message MSG_POS_ECEF (0x0209).The position solution message reports absolute Earth Centered Earth Fixed (ECEF) coordinates and the status (single point vs pseudo-absolute RTK) of the position solution. If the rover receiver knows the surveyed position of the base station and has an RTK solution, this reports a pseudo-absolute position solution using the base station position and the rover's RTK baseline vector. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow).hGPS Time of WeekiECEF X coordinatejECEF Y coordinatekECEF Z coordinatel%Position estimated standard deviationm%Number of satellites used in solutionn Status flags~0SBP class for message MSG_POS_ECEF_COV (0x0214).4The position solution message reports absolute Earth Centered Earth Fixed (ECEF) coordinates and the status (single point vs pseudo-absolute RTK) of the position solution. The message also reports the upper triangular portion of the 3x3 covariance matrix. If the receiver knows the surveyed position of the base station and has an RTK solution, this reports a pseudo-absolute position solution using the base station position and the rover's RTK baseline vector. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow).GPS Time of WeekECEF X coordinateECEF Y coordinateECEF Z coordinateEstimated variance of xEstimated covariance of x and yEstimated covariance of x and zEstimated variance of yEstimated covariance of y and zEstimated variance of z%Number of satellites used in solution Status flags+SBP class for message MSG_POS_LLH (0x020A).This position solution message reports the absolute geodetic coordinates and the status (single point vs pseudo-absolute RTK) of the position solution. If the rover receiver knows the surveyed position of the base station and has an RTK solution, this reports a pseudo-absolute position solution using the base station position and the rover's RTK baseline vector. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow).GPS Time of WeekLatitude LongitudeHeight above WGS84 ellipsoid0Horizontal position estimated standard deviation.Vertical position estimated standard deviation&Number of satellites used in solution. Status flags/SBP class for message MSG_POS_LLH_COV (0x0211).)This position solution message reports the absolute geodetic coordinates and the status (single point vs pseudo-absolute RTK) of the position solution as well as the upper triangle of the 3x3 covariance matrix. The position information and Fix Mode flags should follow the MSG_POS_LLH message. Since the covariance matrix is computed in the local-level North, East, Down frame, the covariance terms follow with that convention. Thus, covariances are reported against the "downward" measurement and care should be taken with the sign convention.GPS Time of WeekLatitude LongitudeHeight above WGS84 ellipsoidEstimated variance of northing"Covariance of northing and easting/Covariance of northing and downward measurementEstimated variance of easting.Covariance of easting and downward measurement*Estimated variance of downward measurement&Number of satellites used in solution. Status flags1SBP class for message MSG_BASELINE_ECEF (0x020B).This message reports the baseline solution in Earth Centered Earth Fixed (ECEF) coordinates. This baseline is the relative vector distance from the base station to the rover receiver. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow).GPS Time of WeekBaseline ECEF X coordinateBaseline ECEF Y coordinateBaseline ECEF Z coordinate%Position estimated standard deviation%Number of satellites used in solution Status flags0SBP class for message MSG_BASELINE_NED (0x020C).~This message reports the baseline solution in North East Down (NED) coordinates. This baseline is the relative vector distance from the base station to the rover receiver, and NED coordinate system is defined at the local WGS84 tangent plane centered at the base station position. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of- week (tow).GPS Time of WeekBaseline North coordinateBaseline East coordinateBaseline Down coordinate0Horizontal position estimated standard deviation.Vertical position estimated standard deviation%Number of satellites used in solution Status flags ,SBP class for message MSG_VEL_ECEF (0x020D).This message reports the velocity in Earth Centered Earth Fixed (ECEF) coordinates. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow).GPS Time of WeekVelocity ECEF X coordinateVelocity ECEF Y coordinateVelocity ECEF Z coordinate%Velocity estimated standard deviation%Number of satellites used in solution Status flags&0SBP class for message MSG_VEL_ECEF_COV (0x0215).This message reports the velocity in Earth Centered Earth Fixed (ECEF) coordinates. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow).(GPS Time of Week)Velocity ECEF X coordinate*Velocity ECEF Y coordinate+Velocity ECEF Z coordinate,Estimated variance of x-Estimated covariance of x and y.Estimated covariance of x and z/Estimated variance of y0Estimated covariance of y and z1Estimated variance of z2%Number of satellites used in solution3 Status flagsC+SBP class for message MSG_VEL_NED (0x020E).This message reports the velocity in local North East Down (NED) coordinates. The NED coordinate system is defined as the local WGS84 tangent plane centered at the current position. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow).EGPS Time of WeekFVelocity North coordinateGVelocity East coordinateHVelocity Down coordinateI0Horizontal velocity estimated standard deviationJ.Vertical velocity estimated standard deviationK%Number of satellites used in solutionL Status flagsa/SBP class for message MSG_VEL_NED_COV (0x0212).This message reports the velocity in local North East Down (NED) coordinates. The NED coordinate system is defined as the local WGS84 tangent plane centered at the current position. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow). This message is similar to the MSG_VEL_NED, but it includes the upper triangular portion of the 3x3 covariance matrix.cGPS Time of WeekdVelocity North coordinateeVelocity East coordinatefVelocity Down coordinateg+Estimated variance of northward measurementh0Covariance of northward and eastward measurementi0Covariance of northward and downward measurementj*Estimated variance of eastward measurementk/Covariance of eastward and downward measurementl*Estimated variance of downward measurementm%Number of satellites used in solutionn Status flags,SBP class for message MSG_VEL_BODY (0x0213).This message reports the velocity in the Vehicle Body Frame. By convention, the x-axis should point out the nose of the vehicle and represent the forward direction, while as the y-axis should point out the right hand side of the vehicle. Since this is a right handed system, z should point out the bottom of the vehicle. The orientation and origin of the Vehicle Body Frame are specified via the device settings. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow).GPS Time of WeekVelocity in x directionVelocity in y directionVelocity in z directionEstimated variance of xCovariance of x and yCovariance of x and zEstimated variance of yCovariance of y and zEstimated variance of z%Number of satellites used in solution Status flags3SBP class for message MSG_AGE_CORRECTIONS (0x0210).[This message reports the Age of the corrections used for the current Differential solutionGPS Time of Week1Age of the corrections (0xFFFF indicates invalid)2SBP class for message MSG_GPS_TIME_DEP_A (0x0100).This message reports the GPS time, representing the time since the GPS epoch began on midnight January 6, 1980 UTC. GPS time counts the weeks and seconds of the week. The weeks begin at the Saturday/Sunday transition. GPS week 0 began at the beginning of the GPS time scale. Within each week number, the GPS time of the week is between between 0 and 604800 seconds (=60*60*24*7). Note that GPS time does not accumulate leap seconds, and as of now, has a small offset from UTC. In a message stream, this message precedes a set of other navigation messages referenced to the same time (but lacking the ns field) and indicates a more precise time of these messages.GPS week number3GPS time of week rounded to the nearest millisecondONanosecond residual of millisecond-rounded TOW (ranges from -500000 to 500000)Status flags (reserved).SBP class for message MSG_DOPS_DEP_A (0x0206).This dilution of precision (DOP) message describes the effect of navigation satellite geometry on positional measurement precision.GPS Time of WeekGeometric Dilution of PrecisionPosition Dilution of PrecisionTime Dilution of Precision Horizontal Dilution of PrecisionVertical Dilution of Precision2SBP class for message MSG_POS_ECEF_DEP_A (0x0200).The position solution message reports absolute Earth Centered Earth Fixed (ECEF) coordinates and the status (single point vs pseudo-absolute RTK) of the position solution. If the rover receiver knows the surveyed position of the base station and has an RTK solution, this reports a pseudo-absolute position solution using the base station position and the rover's RTK baseline vector. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow).GPS Time of WeekECEF X coordinateECEF Y coordinateECEF Z coordinate<Position accuracy estimate (not implemented). Defaults to 0.%Number of satellites used in solution Status flags1SBP class for message MSG_POS_LLH_DEP_A (0x0201).This position solution message reports the absolute geodetic coordinates and the status (single point vs pseudo-absolute RTK) of the position solution. If the rover receiver knows the surveyed position of the base station and has an RTK solution, this reports a pseudo-absolute position solution using the base station position and the rover's RTK baseline vector. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow).GPS Time of WeekLatitude LongitudeHeightGHorizontal position accuracy estimate (not implemented). Defaults to 0.EVertical position accuracy estimate (not implemented). Defaults to 0.&Number of satellites used in solution. Status flags 7SBP class for message MSG_BASELINE_ECEF_DEP_A (0x0202).This message reports the baseline solution in Earth Centered Earth Fixed (ECEF) coordinates. This baseline is the relative vector distance from the base station to the rover receiver. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow).GPS Time of WeekBaseline ECEF X coordinateBaseline ECEF Y coordinateBaseline ECEF Z coordinatePosition accuracy estimate%Number of satellites used in solution Status flags&6SBP class for message MSG_BASELINE_NED_DEP_A (0x0203).~This message reports the baseline solution in North East Down (NED) coordinates. This baseline is the relative vector distance from the base station to the rover receiver, and NED coordinate system is defined at the local WGS84 tangent plane centered at the base station position. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of- week (tow).(GPS Time of Week)Baseline North coordinate*Baseline East coordinate+Baseline Down coordinate,GHorizontal position accuracy estimate (not implemented). Defaults to 0.-EVertical position accuracy estimate (not implemented). Defaults to 0..%Number of satellites used in solution/ Status flags?2SBP class for message MSG_VEL_ECEF_DEP_A (0x0204).This message reports the velocity in Earth Centered Earth Fixed (ECEF) coordinates. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow).AGPS Time of WeekBVelocity ECEF X coordinateCVelocity ECEF Y coordinateDVelocity ECEF Z coordinateE<Velocity accuracy estimate (not implemented). Defaults to 0.F%Number of satellites used in solutionGStatus flags (reserved)X1SBP class for message MSG_VEL_NED_DEP_A (0x0205).This message reports the velocity in local North East Down (NED) coordinates. The NED coordinate system is defined as the local WGS84 tangent plane centered at the current position. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow).ZGPS Time of Week[Velocity North coordinate\Velocity East coordinate]Velocity Down coordinate^GHorizontal velocity accuracy estimate (not implemented). Defaults to 0._EVertical velocity accuracy estimate (not implemented). Defaults to 0.`%Number of satellites used in solutionaStatus flags (reserved)q:SBP class for message MSG_BASELINE_HEADING_DEP_A (0x0207).This message reports the baseline heading pointing from the base station to the rover relative to True North. The full GPS time is given by the preceding MSG_GPS_TIME with the matching time-of-week (tow).sGPS Time of WeektHeadingu%Number of satellites used in solutionv Status flags'()*+,-56789:;<=>?@ABCDLMNOPQRSTUVWXYZ[\]^fghijklmnopqrstuv~ &'()*+,-./0123456789:;CDEFGHIJKLMNOPQRSTUVWXYabcdefghijklmnopqrstuvw &'()*+,-./01234567?@ABCDEFGHIJKLMNOPXYZ[\]^_`abcdefghiqrstuvwxyz{|}~-'()*+,.233CBA@D56789:;<=>?EIJJ]\[ZYXWVU^LMNOPQRST_cddutsrqpovfghijklmnw{||~    #$$:987654;&'()*+,-./0123<@AAXWVUTSRQPONMYCDEFGHIJKLZ^__vutsrqpowabcdefghijklmnx|}}    #$$65432107&'()*+,-./8<==ONMLKJIHP?@ABCDEFGQUVVhgfedcbiXYZ[\]^_`ajnoo~}|{zyxwqrstuv'()*+,5 6789:;<=>?LMNOPQRSTfghijklmn~     & '()*+,-./0123C DEFGHIJKLa bcdefghijklmn   & '()*+,-./?@ABCDEFGX YZ[\]^_`aqrstuv.Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#d+SBP class for message MSG_MAG_RAW (0x0902).Raw data from the magnetometer.^Milliseconds since start of GPS week. If the high bit is set, the time is unknown or invalid.5Milliseconds since start of GPS week, fractional part'Magnetic field in the body frame X axis'Magnetic field in the body frame Y axis'Magnetic field in the body frame Z axis .Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#w 'SBP class for message MSG_LOG (0x0401).This message contains a human-readable payload string from the device containing errors, warnings and informational messages at ERROR, WARNING, DEBUG, INFO logging levels. Logging levelHuman-readable string'SBP class for message MSG_FWD (0x0402).This message provides the ability to forward messages over SBP. This may take the form of wrapping up SBP messages received by Piksi for logging purposes or wrapping another protocol with SBP. The source identifier indicates from what interface a forwarded stream derived. The protocol identifier identifies what the expected protocol the forwarded msg contains. Protocol 0 represents SBP and the remaining values are implementation defined.source identifierprotocol identifier&variable length wrapped binary message)SBP class for message MSG_TWEET (0x0012).All the news fit to tweet.Human-readable string-SBP class for message MSG_PRINT_DEP (0x0010). Deprecated.Human-readable string* .Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#G +SBP class for message MSG_IMU_RAW (0x0900).Raw data from the Inertial Measurement Unit, containing accelerometer and gyroscope readings. The sense of the measurements are to be aligned with the indications on the device itself.^Milliseconds since start of GPS week. If the high bit is set, the time is unknown or invalid.5Milliseconds since start of GPS week, fractional part$Acceleration in the IMU frame X axis$Acceleration in the IMU frame Y axis$Acceleration in the IMU frame Z axis$Angular rate around IMU frame X axis$Angular rate around IMU frame Y axis$Angular rate around IMU frame Z axis+SBP class for message MSG_IMU_AUX (0x0901).1Auxiliary data specific to a particular IMU. The imu_typen field will always be consistent but the rest of the payload is device specific and depends on the value of imu_type.IMU typeRaw IMU temperatureIMU configuration$  .Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"# GnssSignal.JSignal identifier containing constellation, band, and satellite identifier+Constellation-specific satellite identifier#Signal constellation, band and code GnssSignalDep. Deprecated. Constellation-specific satellite identifier. Note: unlike GnssSignal, GPS satellites are encoded as (PRN - 1). Other constellations do not have this offset. #Signal constellation, band and code Reserved GPSTimeDep.A wire-appropriate GPS time, defined as the number of milliseconds since beginning of the week on the Saturday/Sunday transition.$Milliseconds since start of GPS weekGPS week number# GPSTimeSec.lA GPS time, defined as the number of seconds since beginning of the week on the Saturday/Sunday transition.%Seconds since start of GPS week&GPS week number/GPSTime.A wire-appropriate receiver clock time, defined as the time since the beginning of the week on the Saturday/Sunday transition. In most cases, observations are epoch aligned so ns field will be 0.1$Milliseconds since start of GPS week2ONanosecond residual of millisecond-rounded TOW (ranges from -500000 to 500000)3GPS week number< CarrierPhase.Carrier phase measurement in cycles represented as a 40-bit fixed point number with Q32.8 layout, i.e. 32-bits of whole cycles and 8-bits of fractional cycles. This phase has the same sign as the pseudorange.>Carrier phase whole cycles?Carrier phase fractional part(     #$%&'(/012345<=>?@ABIJ:     !!('#$%&)--54/01236::BA@<=>?CGGJI     #$%&/0123<=>? .Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#YIKASBP class for message MSG_TRACKING_STATE_DETAILED_DEP_A (0x0021).zThe tracking message returns a set tracking channel parameters for a single tracking channel useful for debugging issues.MReceiver clock time.NTime of transmission of signal from satellite. TOW only valid when TOW status is decoded or propagated. WN only valid when week number valid flag is set.OGPseudorange observation. Valid only when pseudorange valid flag is set.P[Pseudorange observation standard deviation. Valid only when pseudorange valid flag is set.QjCarrier phase observation with typical sign convention. Valid only when PLL pessimistic lock is achieved.RCarrier-to-Noise densityS~Lock time. It is encoded according to DF402 from the RTCM 10403.2 Amendment 2 specification. Valid values range from 0 to 15.TGNSS signal identifier.UCarrier Doppler frequency.V-Carrier Doppler frequency standard deviation.WaNumber of seconds of continuous tracking. Specifies how much time signal is in continuous track.XATCXO clock offset. Valid only when valid clock valid flag is set.Y@TCXO clock drift. Valid only when valid clock valid flag is set.Z;Early-Prompt (EP) and Prompt-Late (PL) correlators spacing.[=Acceleration. Valid only when acceleration valid flag is set.\Synchronization status flags.]TOW status flags.^Tracking loop status flags._Navigation data status flags.`Parameters sets flags.aMiscellaneous flags.j?SBP class for message MSG_TRACKING_STATE_DETAILED_DEP (0x0011). Deprecated.lReceiver clock time.mTime of transmission of signal from satellite. TOW only valid when TOW status is decoded or propagated. WN only valid when week number valid flag is set.nGPseudorange observation. Valid only when pseudorange valid flag is set.o[Pseudorange observation standard deviation. Valid only when pseudorange valid flag is set.pjCarrier phase observation with typical sign convention. Valid only when PLL pessimistic lock is achieved.qCarrier-to-Noise densityr~Lock time. It is encoded according to DF402 from the RTCM 10403.2 Amendment 2 specification. Valid values range from 0 to 15.sGNSS signal identifier.tCarrier Doppler frequency.u-Carrier Doppler frequency standard deviation.vaNumber of seconds of continuous tracking. Specifies how much time signal is in continuous track.wATCXO clock offset. Valid only when valid clock valid flag is set.x@TCXO clock drift. Valid only when valid clock valid flag is set.y;Early-Prompt (EP) and Prompt-Late (PL) correlators spacing.z=Acceleration. Valid only when acceleration valid flag is set.{Synchronization status flags.|TOW status flags.}Tracking loop status flags.~Navigation data status flags.Parameters sets flags.Miscellaneous flags.TrackingChannelState.RTracking channel state for a specific satellite signal and measured signal power.GNSS signal being tracked'Frequency channel number (GLONASS only)4Carrier-to-Noise density. Zero implies invalid cn0.2SBP class for message MSG_TRACKING_STATE (0x0041).The tracking message returns a variable-length array of tracking channel states. It reports status and carrier-to-noise density measurements for all tracked satellites.Signal tracking channel stateTrackingChannelCorrelation.DStructure containing in-phase and quadrature correlation components.In-phase correlationQuadrature correlation/SBP class for message MSG_TRACKING_IQ (0x002C).VWhen enabled, a tracking channel can output the correlations at each update interval.Tracking channel of originGNSS signal identifier#Early, Prompt and Late correlations3SBP class for message MSG_TRACKING_IQ_DEP (0x001C). Deprecated.Tracking channel of originGNSS signal identifier#Early, Prompt and Late correlationsTrackingChannelStateDepA. Deprecated.Status of tracking channelPRN-1 being trackedCarrier-to-noise density8SBP class for message MSG_TRACKING_STATE_DEP_A (0x0016). Deprecated. Satellite tracking channel stateTrackingChannelStateDepB. Deprecated.Status of tracking channelGNSS signal being trackedCarrier-to-noise density8SBP class for message MSG_TRACKING_STATE_DEP_B (0x0013). Deprecated. Signal tracking channel stateKLMNOPQRSTUVWXYZ[\]^_`abjklmnopqrstuvwxyz{|}~   !"#$,bKLMNOPQRSTUVWXYZ[\]^_`acghhjklmnopqrstuvwxyz{|}~   #"!$ %)**, KLMNOPQRSTUVWXYZ[\]^_`ajklmnopqrstuvwxyz{|}~ .Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#(-CodeBiasesContent.mCode biases are to be added to pseudorange. The corrections are conform with typical RTCMv3 MT1059 and 1065./#Signal constellation, band and code0Code bias value7PhaseBiasesContent.}Phase biases are to be added to carrier phase measurements. The corrections are conform with typical RTCMv3 MT1059 and 1065.9#Signal constellation, band and code:Indicator for integer property;9Indicator for two groups of Wide-Lane(s) integer property<QSignal phase discontinuity counter. Increased for every discontinuity in phase.=Phase bias for specified signalF3SBP class for message MSG_SSR_ORBIT_CLOCK (0x05DC).The precise orbit and clock correction message is to be applied as a delta correction to broadcast ephemeris and is typically an equivalent to the 1060 and 1066 RTCM message typesH%GNSS reference time of the correctionIGNSS signal identifier (16 bit)J/Update interval between consecutive correctionsK{IOD of the SSR correction. A change of Issue Of Data SSR is used to indicate a change in the SSR generating configurationL!Issue of broadcast ephemeris dataMOrbit radial delta correctionNOrbit along delta correctionOOrbit along delta correctionP)Velocity of orbit radial delta correctionQ(Velocity of orbit along delta correctionR(Velocity of orbit cross delta correctionSEC0 polynomial coefficient for correction of broadcast satellite clockTEC1 polynomial coefficient for correction of broadcast satellite clockUEC2 polynomial coefficient for correction of broadcast satellite clockc3SBP class for message MSG_SSR_CODE_BIASES (0x05E1).The precise code biases message is to be added to the pseudorange of the corresponding signal to get corrected pseudorange. It is typically an equivalent to the 1059 and 1065 RTCM message typese%GNSS reference time of the correctionfGNSS signal identifier (16 bit)g/Update interval between consecutive correctionsh{IOD of the SSR correction. A change of Issue Of Data SSR is used to indicate a change in the SSR generating configurationi/Code biases for the different satellite signals4SBP class for message MSG_SSR_PHASE_BIASES (0x05E6).:The precise phase biases message contains the biases to be added to the carrier phase of the corresponding signal to get corrected carrier phase measurement, as well as the satellite yaw angle to be applied to compute the phase wind-up correction. It is typically an equivalent to the 1265 RTCM message types%GNSS reference time of the correctionGNSS signal identifier (16 bit)/Update interval between consecutive corrections{IOD of the SSR correction. A change of Issue Of Data SSR is used to indicate a change in the SSR generating configuration3Indicator for the dispersive phase biases property.?Consistency indicator for Melbourne-Wubbena linear combinationsSatellite yaw angleSatellite yaw angle rate7Phase biases corrections for a satellite being tracked.S-./0789:;<=>?FGHIJKLMNOPQRSTUVWXYZ[cdefghijklmnopqrstuvwxe-./0155?>789:;<=@DDZYXWV[FGHIJKLMNOPQRSTU\`aawvutsrqponmlkjxcdefghiy}~~-./0789:;<=FGHIJKLMNOPQRSTUcdefghi  .Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#',SBP class for message MSG_SBAS_RAW (0x7777).This message is sent once per second per SBAS satellite. ME checks the parity of the data block and sends only blocks that pass the check.GNSS signal identifier.0GPS time-of-week at the start of the data block.SBAS message type (0-63)>Raw SBAS data field of 212 bits (last byte padded with zeros). .Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#-g+SBP class for message MSG_ALMANAC (0x0069).sThis is a legacy message for sending and loading a satellite alamanac onto the Piksi's flash memory from the host.,SBP class for message MSG_SET_TIME (0x0068).]This message sets up timing functionality using a coarse GPS time estimate sent by the host.)SBP class for message MSG_RESET (0x00B6).EThis message from the host resets the Piksi back into the bootloader. Reset flags-SBP class for message MSG_RESET_DEP (0x00B2).EThis message from the host resets the Piksi back into the bootloader..SBP class for message MSG_CW_RESULTS (0x00C0).This is an unused legacy message for result reporting from the CW interference channel on the SwiftNAP. This message will be removed in a future release.,SBP class for message MSG_CW_START (0x00C1).This is an unused legacy message from the host for starting the CW interference channel on the SwiftNAP. This message will be removed in a future release.1SBP class for message MSG_RESET_FILTERS (0x0022).cThis message resets either the DGNSS Kalman filters or Integer Ambiguity Resolution (IAR) process. Filter flags-SBP class for message MSG_INIT_BASE (0x0023).This message initializes the integer ambiguity resolution (IAR) process on the Piksi to use an assumed baseline position between the base station and rover receivers. Warns via MSG_PRINT if there aren't a shared minimum number (4) of satellite observations between the two.0SBP class for message MSG_THREAD_STATE (0x0017).The thread usage message from the device reports real-time operating system (RTOS) thread usage statistics for the named thread. The reported percentage values must be normalized. Thread name (NULL terminated) cPercentage cpu use for this thread. Values range from 0 - 1000 and needs to be renormalized to 100  Free stack space for this thread UARTChannel.Throughput, utilization, and error counts on the RX/TX buffers of this UART channel. The reported percentage values must be normalized.UART transmit throughputUART receive throughputUART CRC error countUART IO error countBUART transmit buffer percentage utilization (ranges from 0 to 255)AUART receive buffer percentage utilization (ranges from 0 to 255)%Period.fStatistics on the period of observations received from the base station. As complete observation sets are received, their time of reception is compared with the prior set''s time of reception. This measurement provides a proxy for link quality as incomplete or missing sets will increase the period. Long periods can cause momentary RTK solution outages.'Average period(Minimum period)Maximum period*'Smoothed estimate of the current period7Latency.Statistics on the latency of observations received from the base station. As observation packets are received their GPS time is compared to the current GPS time calculated locally by the receiver to give a precise measurement of the end-to-end communication latency in the system.9Average latency:Minimum latency;Maximum latency<(Smoothed estimate of the current latencyG.SBP class for message MSG_UART_STATE (0x001D).The UART message reports data latency and throughput of the UART channels providing SBP I/O. On the default Piksi configuration, UARTs A and B are used for telemetry radios, but can also be host access ports for embedded hosts, or other interfaces in future. The reported percentage values must be normalized. Observations latency and period can be used to assess the health of the differential corrections link. Latency provides the timeliness of received base observations while the period indicates their likelihood of transmission.IState of UART AJState of UART BKState of UART FTDI (USB logger)LUART communication latencyMObservation receipt periodZ3SBP class for message MSG_UART_STATE_DEPA (0x0018). Deprecated\State of UART A]State of UART B^State of UART FTDI (USB logger)_UART communication latencym-SBP class for message MSG_IAR_STATE (0x0019).This message reports the state of the Integer Ambiguity Resolution (IAR) process, which resolves unknown integer ambiguities from double-differenced carrier-phase measurements from satellite observations.o0Number of integer ambiguity hypotheses remaining|2SBP class for message MSG_MASK_SATELLITE (0x002B).rThis message allows setting a mask to prevent a particular satellite from being used in various Piksi subsystems.~2Mask of systems that should ignore this satellite.)GNSS signal for which the mask is applied6SBP class for message MSG_MASK_SATELLITE_DEP (0x001B). Deprecated.2Mask of systems that should ignore this satellite.)GNSS signal for which the mask is applied2SBP class for message MSG_DEVICE_MONITOR (0x00B5).This message contains temperature and voltage level measurements from the processor's monitoring system and the RF frontend die temperature if available. Device V_inProcessor V_intProcessor V_auxProcessor temperature#Frontend temperature (if available)/SBP class for message MSG_COMMAND_REQ (0x00B8).Request the recipient to execute an command. Output will be sent in MSG_LOG messages, and the exit code will be returned with MSG_COMMAND_RESP.Sequence numberCommand line to execute0SBP class for message MSG_COMMAND_RESP (0x00B9).oThe response to MSG_COMMAND_REQ with the return code of the command. A return code of zero indicates success.Sequence number Exit code2SBP class for message MSG_COMMAND_OUTPUT (0x00BC).Returns the standard output and standard error of the command requested by MSG_COMMAND_REQ. The sequence number can be used to filter for filtering the correct command.Sequence number)Line of standard output or standard error5SBP class for message MSG_NETWORK_STATE_REQ (0x00BA).bRequest state of Piksi network interfaces. Output will be sent in MSG_NETWORK_STATE_RESP messages6SBP class for message MSG_NETWORK_STATE_RESP (0x00BB).}The state of a network interface on the Piksi. Data is made to reflect output of ifaddrs struct returned by getifaddrs in c.(IPv4 address (all zero when unavailable)IPv4 netmask CIDR notation(IPv6 address (all zero when unavailable)IPv6 netmask CIDR notationNumber of Rx bytesNumber of Tx bytesInterface Name!Interface flags from SIOCGIFFLAGS NetworkUsage.PThe bandwidth usage for each interface can be reported within this struct and utilize multiple fields to fully specify the type of traffic that is being tracked. As either the interval of collection or the collection time may vary, both a timestamp and period field is provided, though may not necessarily be populated with a value.1Duration over which the measurement was collected.Number of bytes handled in total within period)Number of bytes transmitted within period&Number of bytes received within periodInterface Name;SBP class for message MSG_NETWORK_BANDWIDTH_USAGE (0x00BD).2The bandwidth usage, a list of usage by interface. Usage measurement array5SBP class for message MSG_CELL_MODEM_STATUS (0x00BE).If a cell modem is present on a piksi device, this message will be send periodically to update the host on the status of the modem and its various parameters.@Received cell signal strength in dBm, zero translates to unknown8BER as reported by the modem, zero translates to unknown$Unspecified data TBD for this schema&.SBP class for message MSG_SPECAN_DEP (0x0050). Deprecated.( Channel ID)!Receiver time of this observation*"Reference frequency of this packet+'Frequency step of points in this packet,"Reference amplitude of this packet--Amplitude unit value of points in this packet.>Amplitude values (in the above units) of points in this packet:*SBP class for message MSG_SPECAN (0x0051).Spectrum analyzer packet.< Channel ID=!Receiver time of this observation>"Reference frequency of this packet?'Frequency step of points in this packet@"Reference amplitude of this packetA-Amplitude unit value of points in this packetB>Amplitude values (in the above units) of points in this packet    %&'()*+,-./0789:;<=>?@GHIJKLMNOPQRZ[\]^_`abcdemnopqrst|}~     &'()*+,-./012:;<=>?@ABCDEFGHIJRSTUVWXR     ##0/.-,+%&'()*155@?>=789:;<AEEQPONRGHIJKLMSWXXdcba`eZ[\]^_fjkksrqptmnouyzz|}~     #$$10/2&'()*+,-.3788IHGFEDCJ:;<=>?@ABKOPPXWVUTSR   %&'()*789:;<GHIJKLMZ[\]^_mno|}~   &'()*+,-.:;<=>?@AB.Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#+RaYObservationHeader.%Header of a GNSS observation message.[GNSS time of this observation\Total number of observations. First nibble is the size of the sequence (n), second nibble is the zero-indexed counter (ith packet of n)cDoppler.Doppler measurement in Hz represented as a 24-bit fixed point number with Q16.8 layout, i.e. 16-bits of whole doppler and 8-bits of fractional doppler. This doppler is defined as positive for approaching satellites.eDoppler whole HzfDoppler fractional partoPackedObsContent.Pseudorange and carrier phase observation for a satellite being tracked. The observations are interoperable with 3rd party receivers and conform with typical RTCMv3 GNSS observations.qPseudorange observationr7Carrier phase observation with typical sign convention.s1Doppler observation with typical sign convention.t4Carrier-to-Noise density. Zero implies invalid cn0.unLock timer. This value gives an indication of the time for which a signal has maintained continuous phase lock. Whenever a signal has lost and regained lock, this value is reset to zero. It is encoded according to DF402 from the RTCM 10403.2 Amendment 2 specification. Valid values range from 0 to 15 and the most significant nibble is reserved for future use.vMeasurement status flags. A bit field of flags providing the status of this observation. If this field is 0 it means only the Cn0 estimate for the signal is valid.wGNSS signal identifier (16 bit)'SBP class for message MSG_OBS (0x004A).The GPS observations message reports all the raw pseudorange and carrier phase observations for the satellites being tracked by the device. Carrier phase observation here is represented as a 40-bit fixed point number with Q32.8 layout (i.e. 32-bits of whole cycles and 8-bits of fractional cycles). The observations are be interoperable with 3rd party receivers and conform with typical RTCMv3 GNSS observations.#Header of a GPS observation messageHPseudorange and carrier phase observation for a satellite being tracked.0SBP class for message MSG_BASE_POS_LLH (0x0044).%The base station position message is the position reported by the base station itself. It is used for pseudo-absolute RTK positioning, and is required to be a high-accuracy surveyed location of the base station. Any error here will result in an error in the pseudo-absolute position output.Latitude LongitudeHeight1SBP class for message MSG_BASE_POS_ECEF (0x0048).ZThe base station position message is the position reported by the base station itself in absolute Earth Centered Earth Fixed coordinates. It is used for pseudo-absolute RTK positioning, and is required to be a high- accuracy surveyed location of the base station. Any error here will result in an error in the pseudo-absolute position output.ECEF X coodinateECEF Y coordinateECEF Z coordinateGNSS signal identifier (16 bit)Time of EphemeridesUser Range AccuracyCurve fit interval+Status of ephemeris, 1 = valid, 0 = invalidSatellite health status. GPS: ICD-GPS-200, chapter 20.3.3.3.1.4 SBAS: 0 = valid, non-zero = invalid GLO: 0 = valid, non-zero = invalidGNSS signal identifierTime of EphemeridesUser Range AccuracyCurve fit interval+Status of ephemeris, 1 = valid, 0 = invalidSatellite health status. GPS: ICD-GPS-200, chapter 20.3.3.3.1.4 SBAS: 0 = valid, non-zero = invalid GLO: 0 = valid, non-zero = invalid7SBP class for message MSG_EPHEMERIS_GPS_DEP_E (0x0081).The ephemeris message returns a set of satellite orbit parameters that is used to calculate GPS satellite position, velocity, and clock offset. Please see the Navstar GPS Space Segment/Navigation user interfaces (ICD-GPS-200, Table 20-III) for more details.%Values common for all ephemeris types*Group delay differential between L1 and L2BAmplitude of the sine harmonic correction term to the orbit radiusDAmplitude of the cosine harmonic correction term to the orbit radiusMAmplitude of the cosine harmonic correction term to the argument of latitudeKAmplitude of the sine harmonic correction term to the argument of latitudeMAmplitude of the cosine harmonic correction term to the angle of inclinationKAmplitude of the sine harmonic correction term to the angle of inclinationMean motion differenceMean anomaly at reference timeEccentricity of satellite orbit+Square root of the semi-major axis of orbit:Longitude of ascending node of orbit plane at weekly epochRate of right ascensionArgument of perigee InclinationInclination first derivative4Polynomial clock correction coefficient (clock bias)5Polynomial clock correction coefficient (clock drift)=Polynomial clock correction coefficient (rate of clock drift)Clock referenceIssue of ephemeris dataIssue of clock data1SBP class for message MSG_EPHEMERIS_GPS (0x0086).The ephemeris message returns a set of satellite orbit parameters that is used to calculate GPS satellite position, velocity, and clock offset. Please see the Navstar GPS Space Segment/Navigation user interfaces (ICD-GPS-200, Table 20-III) for more details.%Values common for all ephemeris types*Group delay differential between L1 and L2BAmplitude of the sine harmonic correction term to the orbit radiusDAmplitude of the cosine harmonic correction term to the orbit radiusMAmplitude of the cosine harmonic correction term to the argument of latitudeKAmplitude of the sine harmonic correction term to the argument of latitudeMAmplitude of the cosine harmonic correction term to the angle of inclinationKAmplitude of the sine harmonic correction term to the angle of inclinationMean motion difference Mean anomaly at reference time Eccentricity of satellite orbit +Square root of the semi-major axis of orbit :Longitude of ascending node of orbit plane at weekly epoch Rate of right ascensionArgument of perigee InclinationInclination first derivative4Polynomial clock correction coefficient (clock bias)5Polynomial clock correction coefficient (clock drift)=Polynomial clock correction coefficient (rate of clock drift)Clock referenceIssue of ephemeris dataIssue of clock data8%Values common for all ephemeris types9Position of the GEO at time toe:Velocity of the GEO at time toe;#Acceleration of the GEO at time toe<5Time offset of the GEO clock w.r.t. SBAS Network Time=/Drift of the GEO clock w.r.t. SBAS Network Time]7SBP class for message MSG_EPHEMERIS_GLO_DEP_A (0x0083).The ephemeris message returns a set of satellite orbit parameters that is used to calculate GLO satellite position, velocity, and clock offset. Please see the GLO ICD 5.1 "Table 4.5 Characteristics of words of immediate information (ephemeris parameters)" for more details._%Values common for all ephemeris types`>Relative deviation of predicted carrier frequency from nominalaCorrection to the SV timeb7Position of the SV at tb in PZ-90.02 coordinates systemc>Velocity vector of the SV at tb in PZ-90.02 coordinates systemd?Acceleration vector of the SV at tb in PZ-90.02 coordinates sysu%Values common for all ephemeris typesvPosition of the GEO at time toewVelocity of the GEO at time toex#Acceleration of the GEO at time toey5Time offset of the GEO clock w.r.t. SBAS Network Timez/Drift of the GEO clock w.r.t. SBAS Network Time7SBP class for message MSG_EPHEMERIS_GLO_DEP_B (0x0085).The ephemeris message returns a set of satellite orbit parameters that is used to calculate GLO satellite position, velocity, and clock offset. Please see the GLO ICD 5.1 "Table 4.5 Characteristics of words of immediate information (ephemeris parameters)" for more details.%Values common for all ephemeris types>Relative deviation of predicted carrier frequency from nominalCorrection to the SV time7Position of the SV at tb in PZ-90.02 coordinates system>Velocity vector of the SV at tb in PZ-90.02 coordinates system?Acceleration vector of the SV at tb in PZ-90.02 coordinates sys7SBP class for message MSG_EPHEMERIS_GLO_DEP_C (0x0087).The ephemeris message returns a set of satellite orbit parameters that is used to calculate GLO satellite position, velocity, and clock offset. Please see the GLO ICD 5.1 "Table 4.5 Characteristics of words of immediate information (ephemeris parameters)" for more details.%Values common for all ephemeris types>Relative deviation of predicted carrier frequency from nominalCorrection to the SV time!Equipment delay between L1 and L27Position of the SV at tb in PZ-90.02 coordinates system>Velocity vector of the SV at tb in PZ-90.02 coordinates system?Acceleration vector of the SV at tb in PZ-90.02 coordinates sys>Frequency slot. FCN+8 (that is [1..14]). 0 or 0xFF for invalid1SBP class for message MSG_EPHEMERIS_GLO (0x0088).The ephemeris message returns a set of satellite orbit parameters that is used to calculate GLO satellite position, velocity, and clock offset. Please see the GLO ICD 5.1 "Table 4.5 Characteristics of words of immediate information (ephemeris parameters)" for more details.%Values common for all ephemeris types>Relative deviation of predicted carrier frequency from nominalCorrection to the SV time!Equipment delay between L1 and L27Position of the SV at tb in PZ-90.02 coordinates system>Velocity vector of the SV at tb in PZ-90.02 coordinates system?Acceleration vector of the SV at tb in PZ-90.02 coordinates sys>Frequency slot. FCN+8 (that is [1..14]). 0 or 0xFF for invalidIssue of ephemeris data3SBP class for message MSG_EPHEMERIS_DEP_D (0x0080).The ephemeris message returns a set of satellite orbit parameters that is used to calculate GPS satellite position, velocity, and clock offset. Please see the Navstar GPS Space Segment/Navigation user interfaces (ICD-GPS-200, Table 20-III) for more details.*Group delay differential between L1 and L2BAmplitude of the sine harmonic correction term to the orbit radiusDAmplitude of the cosine harmonic correction term to the orbit radiusMAmplitude of the cosine harmonic correction term to the argument of latitudeKAmplitude of the sine harmonic correction term to the argument of latitudeMAmplitude of the cosine harmonic correction term to the angle of inclinationKAmplitude of the sine harmonic correction term to the angle of inclinationMean motion differenceMean anomaly at reference timeEccentricity of satellite orbit+Square root of the semi-major axis of orbit:Longitude of ascending node of orbit plane at weekly epochRate of right ascensionArgument of perigee InclinationInclination first derivative4Polynomial clock correction coefficient (clock bias)5Polynomial clock correction coefficient (clock drift)=Polynomial clock correction coefficient (rate of clock drift) Time of week Week numberClock reference time of weekClock reference week number Is valid?Satellite is healthy?GNSS signal identifierIssue of ephemeris dataIssue of clock dataReserved field 3SBP class for message MSG_EPHEMERIS_DEP_A (0x001A). Deprecated. *Group delay differential between L1 and L2 BAmplitude of the sine harmonic correction term to the orbit radius DAmplitude of the cosine harmonic correction term to the orbit radius MAmplitude of the cosine harmonic correction term to the argument of latitude KAmplitude of the sine harmonic correction term to the argument of latitude MAmplitude of the cosine harmonic correction term to the angle of inclination KAmplitude of the sine harmonic correction term to the angle of inclination Mean motion difference Mean anomaly at reference time Eccentricity of satellite orbit +Square root of the semi-major axis of orbit :Longitude of ascending node of orbit plane at weekly epoch Rate of right ascension Argument of perigee  Inclination Inclination first derivative 4Polynomial clock correction coefficient (clock bias) 5Polynomial clock correction coefficient (clock drift) =Polynomial clock correction coefficient (rate of clock drift)  Time of week  Week number Clock reference time of week Clock reference week number  Is valid? Satellite is healthy? PRN being tracked C3SBP class for message MSG_EPHEMERIS_DEP_B (0x0046). Deprecated. E*Group delay differential between L1 and L2 FBAmplitude of the sine harmonic correction term to the orbit radius GDAmplitude of the cosine harmonic correction term to the orbit radius HMAmplitude of the cosine harmonic correction term to the argument of latitude IKAmplitude of the sine harmonic correction term to the argument of latitude JMAmplitude of the cosine harmonic correction term to the angle of inclination KKAmplitude of the sine harmonic correction term to the angle of inclination LMean motion difference MMean anomaly at reference time NEccentricity of satellite orbit O+Square root of the semi-major axis of orbit P:Longitude of ascending node of orbit plane at weekly epoch QRate of right ascension RArgument of perigee S Inclination TInclination first derivative U4Polynomial clock correction coefficient (clock bias) V5Polynomial clock correction coefficient (clock drift) W=Polynomial clock correction coefficient (rate of clock drift) X Time of week Y Week number ZClock reference time of week [Clock reference week number \ Is valid? ]Satellite is healthy? ^PRN being tracked _Issue of ephemeris data 3SBP class for message MSG_EPHEMERIS_DEP_C (0x0047).The ephemeris message returns a set of satellite orbit parameters that is used to calculate GPS satellite position, velocity, and clock offset. Please see the Navstar GPS Space Segment/Navigation user interfaces (ICD-GPS-200, Table 20-III) for more details. *Group delay differential between L1 and L2 BAmplitude of the sine harmonic correction term to the orbit radius DAmplitude of the cosine harmonic correction term to the orbit radius MAmplitude of the cosine harmonic correction term to the argument of latitude KAmplitude of the sine harmonic correction term to the argument of latitude MAmplitude of the cosine harmonic correction term to the angle of inclination KAmplitude of the sine harmonic correction term to the angle of inclination Mean motion difference Mean anomaly at reference time Eccentricity of satellite orbit +Square root of the semi-major axis of orbit :Longitude of ascending node of orbit plane at weekly epoch Rate of right ascension Argument of perigee  Inclination Inclination first derivative 4Polynomial clock correction coefficient (clock bias) 5Polynomial clock correction coefficient (clock drift) =Polynomial clock correction coefficient (rate of clock drift)  Time of week  Week number Clock reference time of week Clock reference week number  Is valid? Satellite is healthy? GNSS signal identifier Issue of ephemeris data Issue of clock data Reserved field ObservationHeaderDep.$Header of a GPS observation message. GPS time of this observation Total number of observations. First nibble is the size of the sequence (n), second nibble is the zero-indexed counter (ith packet of n) CarrierPhaseDepA.Carrier phase measurement in cycles represented as a 40-bit fixed point number with Q32.8 layout, i.e. 32-bits of whole cycles and 8-bits of fractional cycles. This has the opposite sign convention than a typical GPS receiver and the phase has the opposite sign as the pseudorange. Carrier phase whole cycles Carrier phase fractional part PackedObsContentDepA. Deprecated. Pseudorange observation DCarrier phase observation with opposite sign from typical convention Carrier-to-Noise density Lock indicator. This value changes whenever a satellite signal has lost and regained lock, indicating that the carrier phase ambiguity may have changed. (PRN-1 identifier of the satellite signal PackedObsContentDepB.Pseudorange and carrier phase observation for a satellite being tracked. Pseudoranges are referenced to a nominal pseudorange. Pseudorange observation ECarrier phase observation with opposite sign from typical convention. Carrier-to-Noise density Lock indicator. This value changes whenever a satellite signal has lost and regained lock, indicating that the carrier phase ambiguity may have changed. GNSS signal identifier PackedObsContentDepC.Pseudorange and carrier phase observation for a satellite being tracked. The observations are be interoperable with 3rd party receivers and conform with typical RTCMv3 GNSS observations. Pseudorange observation 7Carrier phase observation with typical sign convention. Carrier-to-Noise density Lock indicator. This value changes whenever a satellite signal has lost and regained lock, indicating that the carrier phase ambiguity may have changed. GNSS signal identifier *-SBP class for message MSG_OBS_DEP_A (0x0045). Deprecated. ,#Header of a GPS observation message -HPseudorange and carrier phase observation for a satellite being tracked. ;-SBP class for message MSG_OBS_DEP_B (0x0043).This observation message has been deprecated in favor of observations that are more interoperable. This message should be used for observations referenced to a nominal pseudorange which are not interoperable with most 3rd party GNSS receievers or typical RTCMv3 observations. =#Header of a GPS observation message >HPseudorange and carrier phase observation for a satellite being tracked. I-SBP class for message MSG_OBS_DEP_C (0x0049).The GPS observations message reports all the raw pseudorange and carrier phase observations for the satellites being tracked by the device. Carrier phase observation here is represented as a 40-bit fixed point number with Q32.8 layout (i.e. 32-bits of whole cycles and 8-bits of fractional cycles). The observations are interoperable with 3rd party receivers and conform with typical RTCMv3 GNSS observations. K#Header of a GPS observation message LHPseudorange and carrier phase observation for a satellite being tracked. W(SBP class for message MSG_IONO (0x0090).The ionospheric parameters which allow the "L1 only" or "L2 only" user to utilize the ionospheric model for computation of the ionospheric delay. Please see ICD-GPS-200 (Chapter 20.3.3.5.1.7) for more details. Y1Navigation Message Correction Table Valitidy Time l8SBP class for message MSG_SV_CONFIGURATION_GPS (0x0091).?Please see ICD-GPS-200 (Chapter 20.3.3.5.1.4) for more details. n1Navigation Message Correction Table Valitidy Time o:L2C capability mask, SV32 bit being MSB, SV1 bit being LSB 5SBP class for message MSG_GROUP_DELAY_DEP_A (0x0092).7Please see ICD-GPS-200 (30.3.3.3.1.1) for more details. Data Predict Time of Week Satellite number zbit-field indicating validity of the values, LSB indicating tgd validity etc. 1 = value is valid, 0 = value is not valid. 5SBP class for message MSG_GROUP_DELAY_DEP_B (0x0093).7Please see ICD-GPS-200 (30.3.3.3.1.1) for more details. Data Predict Time of Week GNSS signal identifier zbit-field indicating validity of the values, LSB indicating tgd validity etc. 1 = value is valid, 0 = value is not valid. /SBP class for message MSG_GROUP_DELAY (0x0094).7Please see ICD-GPS-200 (30.3.3.3.1.1) for more details. Data Predict Time of Week GNSS signal identifier zbit-field indicating validity of the values, LSB indicating tgd validity etc. 1 = value is valid, 0 = value is not valid. GNSS signal identifier Reference time of almanac User Range Accuracy Curve fit interval )Status of almanac, 1 = valid, 0 = invalid Satellite health status for GPS: - bits 5-7: NAV data health status. See IS-GPS-200H Table 20-VII: NAV Data Health Indications. - bits 0-4: Signal health status. See IS-GPS-200H Table 20-VIII. Codes for Health of SV Signal Components. Satellite health status for GLO: See GLO ICD 5.1 table 5.1 for details - bit 0: C(n), "unhealthy" flag that is transmitted within non-immediate data and indicates overall constellation status at the moment of almanac uploading. '0', indicates malfunction of n-satellite. '1'@ indicates that n-satellite is operational. - bit 1: Bn(ln), '0'I indicates the satellite is operational and suitable for navigation. GNSS signal identifier Reference time of almanac User Range Accuracy Curve fit interval )Status of almanac, 1 = valid, 0 = invalid Satellite health status for GPS: - bits 5-7: NAV data health status. See IS-GPS-200H Table 20-VII: NAV Data Health Indications. - bits 0-4: Signal health status. See IS-GPS-200H Table 20-VIII. Codes for Health of SV Signal Components. Satellite health status for GLO: See GLO ICD 5.1 table 5.1 for details - bit 0: C(n), "unhealthy" flag that is transmitted within non-immediate data and indicates overall constellation status at the moment of almanac uploading. '0', indicates malfunction of n-satellite. '1'@ indicates that n-satellite is operational. - bit 1: Bn(ln), '0'I indicates the satellite is operational and suitable for navigation. 3SBP class for message MSG_ALMANAC_GPS_DEP (0x0070).The almanac message returns a set of satellite orbit parameters. Almanac data is not very precise and is considered valid for up to several months. Please see the Navstar GPS Space Segment/Navigation user interfaces (ICD- GPS-200, Chapter 20.3.3.5.1.2 Almanac Data) for more details. #Values common for all almanac types Mean anomaly at reference time Eccentricity of satellite orbit +Square root of the semi-major axis of orbit :Longitude of ascending node of orbit plane at weekly epoch Rate of right ascension Argument of perigee  Inclination 4Polynomial clock correction coefficient (clock bias) 5Polynomial clock correction coefficient (clock drift) /SBP class for message MSG_ALMANAC_GPS (0x0072).The almanac message returns a set of satellite orbit parameters. Almanac data is not very precise and is considered valid for up to several months. Please see the Navstar GPS Space Segment/Navigation user interfaces (ICD- GPS-200, Chapter 20.3.3.5.1.2 Almanac Data) for more details. #Values common for all almanac types Mean anomaly at reference time Eccentricity of satellite orbit +Square root of the semi-major axis of orbit :Longitude of ascending node of orbit plane at weekly epoch Rate of right ascension Argument of perigee  Inclination 4Polynomial clock correction coefficient (clock bias) 5Polynomial clock correction coefficient (clock drift) 3SBP class for message MSG_ALMANAC_GLO_DEP (0x0071).The almanac message returns a set of satellite orbit parameters. Almanac data is not very precise and is considered valid for up to several months. Please see the GLO ICD 5.1 "Chapter 4.5 Non-immediate information and almanac" for details. !#Values common for all almanac types "QLongitude of the first ascending node of the orbit in PZ-90.02 coordinate system #(Time of the first ascending node passage $+Value of inclination at instant of t_lambda %0Value of Draconian period at instant of t_lambda &&Rate of change of the Draconian period '#Eccentricity at instant of t_lambda (*Argument of perigee at instant of t_lambda ;/SBP class for message MSG_ALMANAC_GLO (0x0073).The almanac message returns a set of satellite orbit parameters. Almanac data is not very precise and is considered valid for up to several months. Please see the GLO ICD 5.1 "Chapter 4.5 Non-immediate information and almanac" for details. =#Values common for all almanac types >QLongitude of the first ascending node of the orbit in PZ-90.02 coordinate system ?(Time of the first ascending node passage @+Value of inclination at instant of t_lambda A0Value of Draconian period at instant of t_lambda B&Rate of change of the Draconian period C#Eccentricity at instant of t_lambda D*Argument of perigee at instant of t_lambda U.SBP class for message MSG_GLO_BIASES (0x0075).The GLONASS L1/L2 Code-Phase biases allows to perform GPS+GLONASS integer ambiguity resolution for baselines with mixed receiver types (e.g. receiver of different manufacturers) WGLONASS FDMA signals mask XGLONASS L1 C/A Code-Phase Bias YGLONASS L1 P Code-Phase Bias ZGLONASS L2 C/A Code-Phase Bias [GLONASS L2 P Code-Phase Bias YZ[\cdefghopqrstuvwxy      !"#$%&'()*+,-.6789:;<=>?@ABCDEFGHIJKLMNOPQRSTU]^_`abcdefghijkstuvwxyz{|}~                          ! " # $ % & ' ( ) * + , - . / 0 1 2 3 4 5 6 7 8 9 : ; C D E F G H I J K L M N O P Q R S T U V W X Y Z [ \ ] ^ _ ` a b c d e f g h i j k l m n o p q r s t u v w x y z                ! " # * + , - . / 0 1 2 3 ; < = > ? @ A I J K L M N O W X Y Z [ \ ] ^ _ ` a b c d l m n o p q r s t u v w x y                    ! " # $ % & ' ( ) * + , - . / 0 1 2 3 ; < = > ? @ A B C D E F G H I J K L M U V W X Y Z [ \ ] ^ _ ` a b c d l m n o pYZ[\]aahgcdefimmyxopqrstuvwz~~-,+*)('&%$#"! .     /344TSRQPONMLKJIHGFEDCBA@?>U6789:;<=VZ[[jihgfek]^_`abcdlpqq~}|{stuvwxyz : 9 8 7 6 5 4 3 2 1 0 / . - , + * ) ( ' & % $ # " !   ;                        < @ A A y x w v u t s r q p o n m l k j i h g f e d c b a ` z C D E F G H I J K L M N O P Q R S T U V W X Y Z [ \ ] ^ _ {              # " !         $ ( ( 2 1 0 / . 3 * + , - 4 8 9 9 @ ? A ; < = > B F G G N M O I J K L P T U U c b d W X Y Z [ \ ] ^ _ ` a e i j j x w v u t s r q p y l m n o z ~                         2 1 0 / . - , + * ) 3  ! " # $ % & ' ( 4 8 9 9 L K J I H G F E M ; < = > ? @ A B C D N R S S c b a ` _ ^ ] \ d U V W X Y Z [ e i j j p o n m l(YZ[\cdefopqrstuvw     6789:;<=]^_`abcdstuvwxyz                          C D E F G H I J K L M N O P Q R S T U V W X Y Z [ \ ] ^ _               * + , - ; < = > I J K L W X Y Z [ \ ] ^ _ ` a l m n o               ! " # $ % & ' ( ; < = > ? @ A B C D U V W X Y Z [.Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#\/ q-SBP class for message MSG_NDB_EVENT (0x0400).This message is sent out when an object is stored into NDB. If needed message could also be sent out when fetching an object from NDB. sHW time in milliseconds. t Event type. uEvent object type. v Event result. w7Data source for STORE event, reserved for other events. xGNSS signal identifier, If object_type is Ephemeris OR Almanac, sid indicates for which signal the object belongs to. Reserved in other cases. yGNSS signal identifier, If object_type is Almanac, Almanac WN, Iono OR L2C capabilities AND data_source is NDB_DS_RECEIVER sid indicates from which SV data was decoded. Reserved in other cases. zA unique identifier of the sending hardware. For v1.0, set to the 2 least significant bytes of the device serial number, valid only if data_source is NDB_DS_SBP. Reserved in case of other data_source. q r s t u v w x y z {  { q r s t u v w x y z |  q r s t u v w x y z.Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"# 1SBP class for message MSG_FLASH_PROGRAM (0x00E6).bThe flash program message programs a set of addresses of either the STM or M25 flash. The device replies with either a MSG_FLASH_DONE message containing the return code FLASH_OK (0) on success, or FLASH_INVALID_LEN (2) if the maximum write size is exceeded. Note that the sector-containing addresses must be erased before addresses can be programmed.  Target flags "Starting address offset to program HLength of set of addresses to program, counting up from starting address 6Data to program addresses with, with length N=addr_len .SBP class for message MSG_FLASH_DONE (0x00E0).This message defines success or failure codes for a variety of flash memory requests from the host to the device. Flash read and write messages, such as MSG_FLASH_READ_REQ, or MSG_FLASH_PROGRAM, may return this message on failure. Response flags 2SBP class for message MSG_FLASH_READ_REQ (0x00E7).yThe flash read message reads a set of addresses of either the STM or M25 onboard flash. The device replies with a MSG_FLASH_READ_RESP message containing either the read data on success or a MSG_FLASH_DONE message containing the return code FLASH_INVALID_LEN (2) if the maximum read size is exceeded or FLASH_INVALID_ADDR (3) if the address is outside of the allowed range.  Target flags $Starting address offset to read from ELength of set of addresses to read, counting up from starting address 3SBP class for message MSG_FLASH_READ_RESP (0x00E1).yThe flash read message reads a set of addresses of either the STM or M25 onboard flash. The device replies with a MSG_FLASH_READ_RESP message containing either the read data on success or a MSG_FLASH_DONE message containing the return code FLASH_INVALID_LEN (2) if the maximum read size is exceeded or FLASH_INVALID_ADDR (3) if the address is outside of the allowed range.  Target flags $Starting address offset to read from ELength of set of addresses to read, counting up from starting address /SBP class for message MSG_FLASH_ERASE (0x00E2).The flash erase message from the host erases a sector of either the STM or M25 onboard flash memory. The device will reply with a MSG_FLASH_DONE message containing the return code - FLASH_OK (0) on success or FLASH_INVALID_FLASH (1) if the flash specified is invalid.  Target flags AFlash sector number to erase (0-11 for the STM, 0-15 for the M25) 9SBP class for message MSG_STM_FLASH_LOCK_SECTOR (0x00E3).qThe flash lock message locks a sector of the STM flash memory. The device replies with a MSG_FLASH_DONE message. Flash sector number to lock ;SBP class for message MSG_STM_FLASH_UNLOCK_SECTOR (0x00E4).uThe flash unlock message unlocks a sector of the STM flash memory. The device replies with a MSG_FLASH_DONE message. Flash sector number to unlock 5SBP class for message MSG_STM_UNIQUE_ID_REQ (0x00E8).This message reads the device's hardcoded unique ID. The host requests the ID by sending a MSG_STM_UNIQUE_ID_REQ. The device responds with a MSG_STM_UNIQUE_ID_RESP with the 12-byte unique ID in the payload. 6SBP class for message MSG_STM_UNIQUE_ID_RESP (0x00E5).This message reads the device's hardcoded unique ID. The host requests the ID by sending a MSG_STM_UNIQUE_ID_REQ. The device responds with a MSG_STM_UNIQUE_ID_RESP with the 12-byte unique ID in the payload.. Device unique ID :SBP class for message MSG_M25_FLASH_WRITE_STATUS (0x00F3).zThe flash status message writes to the 8-bit M25 flash status register. The device replies with a MSG_FLASH_DONE message. .Byte to write to the M25 flash status register@      h                       .Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#4 3SBP class for message MSG_FILEIO_READ_REQ (0x00A8).The file read message reads a certain length (up to 255 bytes) from a given offset into a file, and returns the data in a MSG_FILEIO_READ_RESP message where the message length field indicates how many bytes were succesfully read.The sequence number in the request will be returned in the response. If the message is invalid, a followup MSG_PRINT message will print "Invalid fileio read message". A device will only respond to this message when it is received from sender ID 0x42. Read sequence number  File offset Chunk size to read Name of the file to read from 4SBP class for message MSG_FILEIO_READ_RESP (0x00A3).The file read message reads a certain length (up to 255 bytes) from a given offset into a file, and returns the data in a message where the message length field indicates how many bytes were succesfully read. The sequence number in the response is preserved from the request. !Read sequence number "Contents of read file /7SBP class for message MSG_FILEIO_READ_DIR_REQ (0x00A9).MThe read directory message lists the files in a directory on the device's onboard flash file system. The offset parameter can be used to skip the first n elements of the file list. Returns a MSG_FILEIO_READ_DIR_RESP message containing the directory listings as a NULL delimited list. The listing is chunked over multiple SBP packets. The sequence number in the request will be returned in the response. If message is invalid, a followup MSG_PRINT message will print "Invalid fileio read message". A device will only respond to this message when it is received from sender ID 0x42. 1Read sequence number 28The offset to skip the first n elements of the file list 3Name of the directory to list >8SBP class for message MSG_FILEIO_READ_DIR_RESP (0x00AA).tThe read directory message lists the files in a directory on the device's onboard flash file system. Message contains the directory listings as a NULL delimited list. The listing is chunked over multiple SBP packets and the end of the list is identified by an entry containing just the character 0xFF. The sequence number in the response is preserved from the request. @Read sequence number AContents of read directory M1SBP class for message MSG_FILEIO_REMOVE (0x00AC).The file remove message deletes a file from the file system. If the message is invalid, a followup MSG_PRINT message will print "Invalid fileio remove message". A device will only process this message when it is received from sender ID 0x42. OName of the file to delete Z4SBP class for message MSG_FILEIO_WRITE_REQ (0x00AD).The file write message writes a certain length (up to 255 bytes) of data to a file at a given offset. Returns a copy of the original MSG_FILEIO_WRITE_RESP message to check integrity of the write. The sequence number in the request will be returned in the response. If message is invalid, a followup MSG_PRINT message will print "Invalid fileio write message". A device will only process this message when it is received from sender ID 0x42. \Write sequence number ]7Offset into the file at which to start writing in bytes ^Name of the file to write to _&Variable-length array of data to write i5SBP class for message MSG_FILEIO_WRITE_RESP (0x00AB).The file write message writes a certain length (up to 255 bytes) of data to a file at a given offset. The message is a copy of the original MSG_FILEIO_WRITE_REQ message to check integrity of the write. The sequence number in the response is preserved from the request. kWrite sequence number7         ! " # $ % & ' / 0 1 2 3 4 5 6 > ? @ A B C D E M N O P Q R Z [ \ ] ^ _ ` a i j k l m n o p xS            & % $ # '  ! " ( , - - 5 4 6 / 0 1 2 3 7 ; < < D C B E > ? @ A F J K K Q P R M N O S W X X ` a Z [ \ ] ^ _ b f g g o n m l p i j k q u v v x        ! " / 0 1 2 3 > ? @ A M N O Z [ \ ] ^ _ i j k.Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#ބ y-SBP class for message MSG_EXT_EVENT (0x0101).yReports detection of an external event, the GPS time it occurred, which pin it was and whether it was rising or falling. {GPS week number |3GPS time of week rounded to the nearest millisecond }ONanosecond residual of millisecond-rounded TOW (ranges from -500000 to 500000) ~Flags Pin number. 0..9 = DEBUG0..9. y z { | } ~   y z { | } ~   y z { | } ~ .Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"# <SBP class for message MSG_BOOTLOADER_HANDSHAKE_REQ (0x00B3).The handshake message request from the host establishes a handshake between the device bootloader and the host. The response from the device is MSG_BOOTLOADER_HANDSHAKE_RESP. =SBP class for message MSG_BOOTLOADER_HANDSHAKE_RESP (0x00B4). The handshake message response from the device establishes a handshake between the device bootloader and the host. The request from the host is MSG_BOOTLOADER_HANDSHAKE_REQ. The payload contains the bootloader version number and the SBP protocol version number. Bootloader flags Bootloader version number :SBP class for message MSG_BOOTLOADER_JUMP_TO_APP (0x00B1).=The host initiates the bootloader to jump to the application. Ignored by the device 6SBP class for message MSG_NAP_DEVICE_DNA_REQ (0x00DE).ZThe device message from the host reads a unique device identifier from the SwiftNAP, an FPGA. The host requests the ID by sending a MSG_NAP_DEVICE_DNA_REQ message. The device responds with a MSG_NAP_DEVICE_DNA_RESP message with the device ID in the payload. Note that this ID is tied to the FPGA, and not related to the Piksi's serial number. 7SBP class for message MSG_NAP_DEVICE_DNA_RESP (0x00DD).]The device message from the host reads a unique device identifier from the SwiftNAP, an FPGA. The host requests the ID by sending a MSG_NAP_DEVICE_DNA_REQ message. The device responds with a MSG_NAP_DEVICE_DNA_RESP messagage with the device ID in the payload. Note that this ID is tied to the FPGA, and not related to the Piksi's serial number. G57-bit SwiftNAP FPGA Device ID. Remaining bits are padded on the right. >SBP class for message MSG_BOOTLOADER_HANDSHAKE_DEP_A (0x00B0). Deprecated. +Version number string (not NULL terminated) 4        .Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#+O2 .SBP class for message MSG_ACQ_RESULT (0x002F). This message describes the results from an attempted GPS signal acquisition search for a satellite PRN over a code phase/carrier frequency range. It contains the parameters of the point in the acquisition search space with the best carrier-to-noise (CN/0) ratio. CN/0 of best point Code phase of best point Carrier frequency of best point /GNSS signal for which acquisition was attempted 4SBP class for message MSG_ACQ_RESULT_DEP_C (0x001F). Deprecated. CN/0 of best point Code phase of best point Carrier frequency of best point /GNSS signal for which acquisition was attempted 4SBP class for message MSG_ACQ_RESULT_DEP_B (0x0014). Deprecated. ySNR of best point. Currently in arbitrary SNR points, but will be in units of dB Hz in a later revision of this message. Code phase of best point Carrier frequency of best point /GNSS signal for which acquisition was attempted 4SBP class for message MSG_ACQ_RESULT_DEP_A (0x0015). Deprecated. iSNR of best point. Currently dimensonless, but will have units of dB Hz in the revision of this message. Code phase of best point Carrier frequency of best point MPRN-1 identifier of the satellite signal for which acquisition was attempted  AcqSvProfile.Profile for a specific SV for debugging purposes The message describes SV profile during acquisition time. The message is used to debug and measure the performance. (SV search job type (deep, fallback, etc) -Acquisition status 1 is Success, 0 is Failure #CN0 value. Only valid if status is '1' Acquisition integration time /GNSS signal for which acquisition was attempted Acq frequency bin width #Timestamp of the job complete event !Time spent to search for sid.code !Doppler range lowest frequency "Doppler range highest frequency #8Doppler value of detected peak. Only valid if status is '1' $4Codephase of detected peak. Only valid if status is '1' /AcqSvProfileDep. Deprecated. 1(SV search job type (deep, fallback, etc) 2-Acquisition status 1 is Success, 0 is Failure 3#CN0 value. Only valid if status is '1' 4Acquisition integration time 5/GNSS signal for which acquisition was attempted 6Acq frequency bin width 7#Timestamp of the job complete event 8!Time spent to search for sid.code 9Doppler range lowest frequency :Doppler range highest frequency ;8Doppler value of detected peak. Only valid if status is '1' <4Codephase of detected peak. Only valid if status is '1' O2SBP class for message MSG_ACQ_SV_PROFILE (0x002E).yThe message describes all SV profiles during acquisition time. The message is used to debug and measure the performance. Q#SV profiles during acquisition time f6SBP class for message MSG_ACQ_SV_PROFILE_DEP (0x001E). Deprecated. h#SV profiles during acquisition timej                ! " # $ % & ' ( / 0 1 2 3 4 5 6 7 8 9 : ; < = > ? @ A B C D E F G H O P Q R S T U V W X Y Z [ \ ] ^ f g h i j r              ( ' & %          ! " # $ ) - - H G F E D C B A @ ? > = / 0 1 2 3 4 5 6 7 8 9 : ; < I M M ] \ [ Z Y X W V U T S R ^ O P Q _ c d d i j f g h k o p p r                 ! " # $ / 0 1 2 3 4 5 6 7 8 9 : ; < O P Q f g h.Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#4 s-SBP class for message MSG_USER_DATA (0x0800).mThis message can contain any application specific user data up to a maximum length of 255 bytes per message. uUser data payload s t u v ~ v s t u w { | | ~ s t u.Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#A ,SBP class for message MSG_ODOMETRY (0x0903).Message representing the x component of vehicle velocity in the user frame at the odometry reference point(s) specified by the user. The offset for the odometry reference point and the definition and origin of the user frame are defined through the device settings interface. There are 4 possible user-defined sources of this message which are labeled arbitrarily source 0 through 3. Time field representing either milliseconds in the GPS Week or local CPU time from the producing system in milliseconds. See the tow_source flag for the exact source of this timestamp. 1The signed forward component of vehicle velocity.  Status flags     .Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNone"#G 8An SBP message ADT composed of all defined SBP messages.Includes SBPMsgUnknown for valid SBP messages with undefined message types and SBPMsgBadCRC for SBP messages with invalid CRC checksums.&       !"#$%&'()*+,-./0123456789:;<=>?@ABCDEFGHIJKLMNOPQRSTUVWXYZ[\]^_`abcdefghijklmnopqrstuvwxyz{|}~       !"#.Copyright (C) 2015-2018 Swift Navigation, Inc.LGPL-3#Swift Navigation <dev@swiftnav.com> experimentalportableNonePS  #$%&'()123456789:;<=>?@AIJKLMNOPQRSTUVWXYZ[\]efghijklmnopqrst|}~&'()*+,-56789:;<=>?@ABCDLMNOPQRSTUVWXYZ[\]^fghijklmnopqrstuv~ &'()*+,-./0123456789:;CDEFGHIJKLMNOPQRSTUVWXYabcdefghijklmnopqrstuvw &'()*+,-./01234567?@ABCDEFGHIJKLMNOPXYZ[\]^_`abcdefghiqrstuvwxyz{|}~     #$%&'(/012345<=>?@ABIJKLMNOPQRSTUVWXYZ[\]^_`abjklmnopqrstuvwxyz{|}~   !"#$,-./0789:;<=>?FGHIJKLMNOPQRSTUVWXYZ[cdefghijklmnopqrstuvwx    %&'()*+,-./0789:;<=>?@GHIJKLMNOPQRZ[\]^_`abcdemnopqrst|}~     &'()*+,-./012:;<=>?@ABCDEFGHIJRSTUVWXYZ[\cdefghopqrstuvwxy      !"#$%&'()*+,-.6789:;<=>?@ABCDEFGHIJKLMNOPQRSTU]^_`abcdefghijkstuvwxyz{|}~                          ! " # $ % & ' ( ) * + , - . / 0 1 2 3 4 5 6 7 8 9 : ; C D E F G H I J K L M N O P Q R S T U V W X Y Z [ \ ] ^ _ ` a b c d e f g h i j k l m n o p q r s t u v w x y z                ! " # * + , - . / 0 1 2 3 ; < = > ? @ A I J K L M N O W X Y Z [ \ ] ^ _ ` a b c d l m n o p q r s t u v w x y                    ! " # $ % & ' ( ) * + , - . / 0 1 2 3 ; < = > ? @ A B C D E F G H I J K L M U V W X Y Z [ \ ] ^ _ ` a b c d l m n o p q r s t u v w x y z {               ! " # $ % & ' / 0 1 2 3 4 5 6 > ? @ A B C D E M N O P Q R Z [ \ ] ^ _ ` a i j k l m n o p x y z { | } ~                 ! 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" # $ % & ' ( ) * + , - . . / 0 1 2 3 4 5 6 7 8 9 : ; < = > ? @ A B C D E F G H I J K L L M N O P Q R S T U V W X Y Z [ \ ] ^ _ ` a b c d e f g h i j k l m n o p q r s t u v w x y z { | } ~                                                                                                                                                                               ! " # $ % & ' ( ) * + , - . / 0 1 2 3 4 5 6 7 8 8 9 : ; < = > ? @ A B C D E F G H I J K L M N O P Q R S T T U V W X Y Z [ \ ] ^ _ ` a b c d e f g h i j k l m n o p q r s t t u v w x y z { | } ~             !"#$%&'()*+,-./01123456789:;<=>??@ABCDEFGHIJKKLMNOPQRSTUVWXXYZ[\]^_`abcdefghhijklmnopqrstuvwxxyz{|}~      !"##$%&'()*+,-./01233456789:;<=>?@ABCDEEFGHIJKLMNOPQRSSTUVWXYZ[\]^_`abbcdefghijklmnopqrrstuvwxyz{|}~      !"#$%&'()*+,-./01223456789:;<=>?@ABCDEFGGHIJKLMNOPQRSTUVWXYZ[\]^^_`abcdefghijklmnopqrstuvwxxyz{|}~                                  ! " # $ % % & ' ( ) * + , - . / 0 1 2 3 4 5 6 7 8 9 : ; < = > ? @ A B C D E F G H I J K L M N O P Q R S T U V W X Y Z [ \ ] ^ _ ` a b c d e f f g h i j k l m n o p q r s t u v w x y z { | } ~                                                                                                                                                                             ! " # $ % & ' ( ) * * + , - . / 0 1 2 3 4 5 6 7 8 9 : ; < = > ? ? @ A B C D E F G H I J K L M N O P Q R S T T U V W X Y Z [ \ ] ^ _ ` a b c d e f g g h i j k l m n o p q r s t u v w x y z z { | } ~                                                                                                                                                                         ! " # $ % % & ' ( ) * + , - . / 0 1 2 3 3 4 5 6 7 8 9 : ; < = > ? @ @ A B C D E F G H I J K L M N O O P Q R S T U V W X Y Z [ \ ] ] ^ _ ` a b c d e f g h i i j k l m n o p q r s t t u v w x y z { | } ~ ~                                                                                                                                                                               ! " # $ % & ' ( ( ) * + , - . / 0 1 2 2 3 4 5 6 7 8 9 : ; < < = > ? @ A B C D E F G H H I J K L M N O P Q R S T U U V W X Y Z [ \ ] ^ _ ` a b c d e f f g h i j k l m n o p q r s t u v w w x y z { | } ~                                                                                                                                                                         ! " # $ % & ' ( ) * + , - . / 0 1 2 3 4 5 6 7 8 9 : ; < = > ? @ A B C D E F G H I J K L M N O P Q R S T U V W X Y Z [ \ ] ^ _ ` a b c d e f g h i j k l m n o p q r s t u v w x y z { | } ~                                                                                                                                       !"!sbp-2.3.15-1bOEr6udiAOJ3lzmr5gZjISwiftNav.CRC16SwiftNav.SBP.TypesSwiftNav.SBP.OrientationSwiftNav.SBP.SystemSwiftNav.SBP.SettingsSwiftNav.SBP.NavigationSwiftNav.SBP.MagSwiftNav.SBP.LoggingSwiftNav.SBP.ImuSwiftNav.SBP.GnssSwiftNav.SBP.TrackingSwiftNav.SBP.SsrSwiftNav.SBP.SbasSwiftNav.SBP.PiksiSwiftNav.SBP.ObservationSwiftNav.SBP.NdbSwiftNav.SBP.FlashSwiftNav.SBP.FileIoSwiftNav.SBP.ExtEventsSwiftNav.SBP.BootloadSwiftNav.SBP.AcquisitionSwiftNav.SBP.UserSwiftNav.SBP.VehicleSwiftNav.SBP.THSwiftNav.SBP.Msg SwiftNav.SBPcrc16Msg _msgSBPType _msgSBPSender _msgSBPLen_msgSBPPayload _msgSBPCrcBytesunBytesmsgSBPPreamble defaultSender $fShowBytes $fReadBytes $fEqBytes $fShowMsg $fReadMsg$fEqMsgToSBPtoSBPHasMsgmsg msgSBPCrc msgSBPLen msgSBPPayload msgSBPSender msgSBPTypecheckCrc $fToJSONMsg $fToJSONBytes $fFromJSONMsg$fFromJSONBytes $fBinaryMsg $fHasMsgMsgMsgBaselineHeading_msgBaselineHeading_tow_msgBaselineHeading_heading_msgBaselineHeading_n_sats_msgBaselineHeading_flagsmsgBaselineHeading$fBinaryMsgBaselineHeading$fShowMsgBaselineHeading$fReadMsgBaselineHeading$fEqMsgBaselineHeading$fToSBPMsgBaselineHeading$fFromJSONMsgBaselineHeading$fToJSONMsgBaselineHeading MsgOrientQuat_msgOrientQuat_tow_msgOrientQuat_w_msgOrientQuat_x_msgOrientQuat_y_msgOrientQuat_z_msgOrientQuat_w_accuracy_msgOrientQuat_x_accuracy_msgOrientQuat_y_accuracy_msgOrientQuat_z_accuracy_msgOrientQuat_flagsmsgBaselineHeading_flagsmsgBaselineHeading_headingmsgBaselineHeading_n_satsmsgBaselineHeading_tow msgOrientQuat$fBinaryMsgOrientQuat$fShowMsgOrientQuat$fReadMsgOrientQuat$fEqMsgOrientQuat$fToSBPMsgOrientQuat$fFromJSONMsgOrientQuat$fToJSONMsgOrientQuatMsgOrientEuler_msgOrientEuler_tow_msgOrientEuler_roll_msgOrientEuler_pitch_msgOrientEuler_yaw_msgOrientEuler_roll_accuracy_msgOrientEuler_pitch_accuracy_msgOrientEuler_yaw_accuracy_msgOrientEuler_flagsmsgOrientQuat_flagsmsgOrientQuat_towmsgOrientQuat_wmsgOrientQuat_w_accuracymsgOrientQuat_xmsgOrientQuat_x_accuracymsgOrientQuat_ymsgOrientQuat_y_accuracymsgOrientQuat_zmsgOrientQuat_z_accuracymsgOrientEuler$fBinaryMsgOrientEuler$fShowMsgOrientEuler$fReadMsgOrientEuler$fEqMsgOrientEuler$fToSBPMsgOrientEuler$fFromJSONMsgOrientEuler$fToJSONMsgOrientEulerMsgAngularRate_msgAngularRate_tow_msgAngularRate_x_msgAngularRate_y_msgAngularRate_z_msgAngularRate_flagsmsgOrientEuler_flagsmsgOrientEuler_pitchmsgOrientEuler_pitch_accuracymsgOrientEuler_rollmsgOrientEuler_roll_accuracymsgOrientEuler_towmsgOrientEuler_yawmsgOrientEuler_yaw_accuracymsgAngularRate$fBinaryMsgAngularRate$fShowMsgAngularRate$fReadMsgAngularRate$fEqMsgAngularRate$fToSBPMsgAngularRate$fFromJSONMsgAngularRate$fToJSONMsgAngularRatemsgAngularRate_flagsmsgAngularRate_towmsgAngularRate_xmsgAngularRate_ymsgAngularRate_z MsgStartup_msgStartup_cause_msgStartup_startup_type_msgStartup_reserved msgStartup$fBinaryMsgStartup$fShowMsgStartup$fReadMsgStartup$fEqMsgStartup$fToSBPMsgStartup$fFromJSONMsgStartup$fToJSONMsgStartupMsgDgnssStatus_msgDgnssStatus_flags_msgDgnssStatus_latency_msgDgnssStatus_num_signals_msgDgnssStatus_sourcemsgStartup_causemsgStartup_reservedmsgStartup_startup_typemsgDgnssStatus$fBinaryMsgDgnssStatus$fShowMsgDgnssStatus$fReadMsgDgnssStatus$fEqMsgDgnssStatus$fToSBPMsgDgnssStatus$fFromJSONMsgDgnssStatus$fToJSONMsgDgnssStatus MsgHeartbeat_msgHeartbeat_flagsmsgDgnssStatus_flagsmsgDgnssStatus_latencymsgDgnssStatus_num_signalsmsgDgnssStatus_source msgHeartbeat$fBinaryMsgHeartbeat$fShowMsgHeartbeat$fReadMsgHeartbeat$fEqMsgHeartbeat$fToSBPMsgHeartbeat$fFromJSONMsgHeartbeat$fToJSONMsgHeartbeat MsgInsStatus_msgInsStatus_flagsmsgHeartbeat_flags msgInsStatus$fBinaryMsgInsStatus$fShowMsgInsStatus$fReadMsgInsStatus$fEqMsgInsStatus$fToSBPMsgInsStatus$fFromJSONMsgInsStatus$fToJSONMsgInsStatusmsgInsStatus_flagsMsgSettingsSavemsgSettingsSave$fBinaryMsgSettingsSave$fShowMsgSettingsSave$fReadMsgSettingsSave$fEqMsgSettingsSave$fToSBPMsgSettingsSave$fFromJSONMsgSettingsSave$fToJSONMsgSettingsSaveMsgSettingsWrite_msgSettingsWrite_settingmsgSettingsWrite$fBinaryMsgSettingsWrite$fShowMsgSettingsWrite$fReadMsgSettingsWrite$fEqMsgSettingsWrite$fToSBPMsgSettingsWrite$fFromJSONMsgSettingsWrite$fToJSONMsgSettingsWriteMsgSettingsWriteResp_msgSettingsWriteResp_status_msgSettingsWriteResp_settingmsgSettingsWrite_settingmsgSettingsWriteResp$fBinaryMsgSettingsWriteResp$fShowMsgSettingsWriteResp$fReadMsgSettingsWriteResp$fEqMsgSettingsWriteResp$fToSBPMsgSettingsWriteResp$fFromJSONMsgSettingsWriteResp$fToJSONMsgSettingsWriteRespMsgSettingsReadReq_msgSettingsReadReq_settingmsgSettingsWriteResp_settingmsgSettingsWriteResp_statusmsgSettingsReadReq$fBinaryMsgSettingsReadReq$fShowMsgSettingsReadReq$fReadMsgSettingsReadReq$fEqMsgSettingsReadReq$fToSBPMsgSettingsReadReq$fFromJSONMsgSettingsReadReq$fToJSONMsgSettingsReadReqMsgSettingsReadResp_msgSettingsReadResp_settingmsgSettingsReadReq_settingmsgSettingsReadResp$fBinaryMsgSettingsReadResp$fShowMsgSettingsReadResp$fReadMsgSettingsReadResp$fEqMsgSettingsReadResp$fToSBPMsgSettingsReadResp$fFromJSONMsgSettingsReadResp$fToJSONMsgSettingsReadRespMsgSettingsReadByIndexReq _msgSettingsReadByIndexReq_indexmsgSettingsReadResp_settingmsgSettingsReadByIndexReq!$fBinaryMsgSettingsReadByIndexReq$fShowMsgSettingsReadByIndexReq$fReadMsgSettingsReadByIndexReq$fEqMsgSettingsReadByIndexReq $fToSBPMsgSettingsReadByIndexReq#$fFromJSONMsgSettingsReadByIndexReq!$fToJSONMsgSettingsReadByIndexReqMsgSettingsReadByIndexResp!_msgSettingsReadByIndexResp_index#_msgSettingsReadByIndexResp_settingmsgSettingsReadByIndexReq_indexmsgSettingsReadByIndexResp"$fBinaryMsgSettingsReadByIndexResp $fShowMsgSettingsReadByIndexResp $fReadMsgSettingsReadByIndexResp$fEqMsgSettingsReadByIndexResp!$fToSBPMsgSettingsReadByIndexResp$$fFromJSONMsgSettingsReadByIndexResp"$fToJSONMsgSettingsReadByIndexRespMsgSettingsReadByIndexDone msgSettingsReadByIndexResp_index"msgSettingsReadByIndexResp_settingmsgSettingsReadByIndexDone"$fBinaryMsgSettingsReadByIndexDone $fShowMsgSettingsReadByIndexDone $fReadMsgSettingsReadByIndexDone$fEqMsgSettingsReadByIndexDone!$fToSBPMsgSettingsReadByIndexDone$$fFromJSONMsgSettingsReadByIndexDone"$fToJSONMsgSettingsReadByIndexDoneMsgSettingsRegister_msgSettingsRegister_settingmsgSettingsRegister$fBinaryMsgSettingsRegister$fShowMsgSettingsRegister$fReadMsgSettingsRegister$fEqMsgSettingsRegister$fToSBPMsgSettingsRegister$fFromJSONMsgSettingsRegister$fToJSONMsgSettingsRegistermsgSettingsRegister_setting MsgGpsTime_msgGpsTime_wn_msgGpsTime_tow_msgGpsTime_ns_residual_msgGpsTime_flags msgGpsTime$fBinaryMsgGpsTime$fShowMsgGpsTime$fReadMsgGpsTime$fEqMsgGpsTime$fToSBPMsgGpsTime$fFromJSONMsgGpsTime$fToJSONMsgGpsTime MsgUtcTime_msgUtcTime_flags_msgUtcTime_tow_msgUtcTime_year_msgUtcTime_month_msgUtcTime_day_msgUtcTime_hours_msgUtcTime_minutes_msgUtcTime_seconds_msgUtcTime_nsmsgGpsTime_flagsmsgGpsTime_ns_residualmsgGpsTime_tow msgGpsTime_wn msgUtcTime$fBinaryMsgUtcTime$fShowMsgUtcTime$fReadMsgUtcTime$fEqMsgUtcTime$fToSBPMsgUtcTime$fFromJSONMsgUtcTime$fToJSONMsgUtcTimeMsgDops _msgDops_tow _msgDops_gdop _msgDops_pdop _msgDops_tdop _msgDops_hdop _msgDops_vdop_msgDops_flagsmsgUtcTime_daymsgUtcTime_flagsmsgUtcTime_hoursmsgUtcTime_minutesmsgUtcTime_month msgUtcTime_nsmsgUtcTime_secondsmsgUtcTime_towmsgUtcTime_yearmsgDops$fBinaryMsgDops $fShowMsgDops $fReadMsgDops $fEqMsgDops$fToSBPMsgDops$fFromJSONMsgDops$fToJSONMsgDops MsgPosEcef_msgPosEcef_tow _msgPosEcef_x _msgPosEcef_y _msgPosEcef_z_msgPosEcef_accuracy_msgPosEcef_n_sats_msgPosEcef_flags msgDops_flags msgDops_gdop msgDops_hdop msgDops_pdop msgDops_tdop msgDops_tow msgDops_vdop msgPosEcef$fBinaryMsgPosEcef$fShowMsgPosEcef$fReadMsgPosEcef$fEqMsgPosEcef$fToSBPMsgPosEcef$fFromJSONMsgPosEcef$fToJSONMsgPosEcef MsgPosEcefCov_msgPosEcefCov_tow_msgPosEcefCov_x_msgPosEcefCov_y_msgPosEcefCov_z_msgPosEcefCov_cov_x_x_msgPosEcefCov_cov_x_y_msgPosEcefCov_cov_x_z_msgPosEcefCov_cov_y_y_msgPosEcefCov_cov_y_z_msgPosEcefCov_cov_z_z_msgPosEcefCov_n_sats_msgPosEcefCov_flagsmsgPosEcef_accuracymsgPosEcef_flagsmsgPosEcef_n_satsmsgPosEcef_tow msgPosEcef_x msgPosEcef_y msgPosEcef_z msgPosEcefCov$fBinaryMsgPosEcefCov$fShowMsgPosEcefCov$fReadMsgPosEcefCov$fEqMsgPosEcefCov$fToSBPMsgPosEcefCov$fFromJSONMsgPosEcefCov$fToJSONMsgPosEcefCov MsgPosLlh_msgPosLlh_tow_msgPosLlh_lat_msgPosLlh_lon_msgPosLlh_height_msgPosLlh_h_accuracy_msgPosLlh_v_accuracy_msgPosLlh_n_sats_msgPosLlh_flagsmsgPosEcefCov_cov_x_xmsgPosEcefCov_cov_x_ymsgPosEcefCov_cov_x_zmsgPosEcefCov_cov_y_ymsgPosEcefCov_cov_y_zmsgPosEcefCov_cov_z_zmsgPosEcefCov_flagsmsgPosEcefCov_n_satsmsgPosEcefCov_towmsgPosEcefCov_xmsgPosEcefCov_ymsgPosEcefCov_z msgPosLlh$fBinaryMsgPosLlh$fShowMsgPosLlh$fReadMsgPosLlh $fEqMsgPosLlh$fToSBPMsgPosLlh$fFromJSONMsgPosLlh$fToJSONMsgPosLlh MsgPosLlhCov_msgPosLlhCov_tow_msgPosLlhCov_lat_msgPosLlhCov_lon_msgPosLlhCov_height_msgPosLlhCov_cov_n_n_msgPosLlhCov_cov_n_e_msgPosLlhCov_cov_n_d_msgPosLlhCov_cov_e_e_msgPosLlhCov_cov_e_d_msgPosLlhCov_cov_d_d_msgPosLlhCov_n_sats_msgPosLlhCov_flagsmsgPosLlh_flagsmsgPosLlh_h_accuracymsgPosLlh_height msgPosLlh_lat msgPosLlh_lonmsgPosLlh_n_sats msgPosLlh_towmsgPosLlh_v_accuracy msgPosLlhCov$fBinaryMsgPosLlhCov$fShowMsgPosLlhCov$fReadMsgPosLlhCov$fEqMsgPosLlhCov$fToSBPMsgPosLlhCov$fFromJSONMsgPosLlhCov$fToJSONMsgPosLlhCovMsgBaselineEcef_msgBaselineEcef_tow_msgBaselineEcef_x_msgBaselineEcef_y_msgBaselineEcef_z_msgBaselineEcef_accuracy_msgBaselineEcef_n_sats_msgBaselineEcef_flagsmsgPosLlhCov_cov_d_dmsgPosLlhCov_cov_e_dmsgPosLlhCov_cov_e_emsgPosLlhCov_cov_n_dmsgPosLlhCov_cov_n_emsgPosLlhCov_cov_n_nmsgPosLlhCov_flagsmsgPosLlhCov_heightmsgPosLlhCov_latmsgPosLlhCov_lonmsgPosLlhCov_n_satsmsgPosLlhCov_towmsgBaselineEcef$fBinaryMsgBaselineEcef$fShowMsgBaselineEcef$fReadMsgBaselineEcef$fEqMsgBaselineEcef$fToSBPMsgBaselineEcef$fFromJSONMsgBaselineEcef$fToJSONMsgBaselineEcefMsgBaselineNed_msgBaselineNed_tow_msgBaselineNed_n_msgBaselineNed_e_msgBaselineNed_d_msgBaselineNed_h_accuracy_msgBaselineNed_v_accuracy_msgBaselineNed_n_sats_msgBaselineNed_flagsmsgBaselineEcef_accuracymsgBaselineEcef_flagsmsgBaselineEcef_n_satsmsgBaselineEcef_towmsgBaselineEcef_xmsgBaselineEcef_ymsgBaselineEcef_zmsgBaselineNed$fBinaryMsgBaselineNed$fShowMsgBaselineNed$fReadMsgBaselineNed$fEqMsgBaselineNed$fToSBPMsgBaselineNed$fFromJSONMsgBaselineNed$fToJSONMsgBaselineNed MsgVelEcef_msgVelEcef_tow _msgVelEcef_x _msgVelEcef_y _msgVelEcef_z_msgVelEcef_accuracy_msgVelEcef_n_sats_msgVelEcef_flagsmsgBaselineNed_dmsgBaselineNed_emsgBaselineNed_flagsmsgBaselineNed_h_accuracymsgBaselineNed_nmsgBaselineNed_n_satsmsgBaselineNed_towmsgBaselineNed_v_accuracy msgVelEcef$fBinaryMsgVelEcef$fShowMsgVelEcef$fReadMsgVelEcef$fEqMsgVelEcef$fToSBPMsgVelEcef$fFromJSONMsgVelEcef$fToJSONMsgVelEcef MsgVelEcefCov_msgVelEcefCov_tow_msgVelEcefCov_x_msgVelEcefCov_y_msgVelEcefCov_z_msgVelEcefCov_cov_x_x_msgVelEcefCov_cov_x_y_msgVelEcefCov_cov_x_z_msgVelEcefCov_cov_y_y_msgVelEcefCov_cov_y_z_msgVelEcefCov_cov_z_z_msgVelEcefCov_n_sats_msgVelEcefCov_flagsmsgVelEcef_accuracymsgVelEcef_flagsmsgVelEcef_n_satsmsgVelEcef_tow msgVelEcef_x msgVelEcef_y msgVelEcef_z msgVelEcefCov$fBinaryMsgVelEcefCov$fShowMsgVelEcefCov$fReadMsgVelEcefCov$fEqMsgVelEcefCov$fToSBPMsgVelEcefCov$fFromJSONMsgVelEcefCov$fToJSONMsgVelEcefCov MsgVelNed_msgVelNed_tow _msgVelNed_n _msgVelNed_e _msgVelNed_d_msgVelNed_h_accuracy_msgVelNed_v_accuracy_msgVelNed_n_sats_msgVelNed_flagsmsgVelEcefCov_cov_x_xmsgVelEcefCov_cov_x_ymsgVelEcefCov_cov_x_zmsgVelEcefCov_cov_y_ymsgVelEcefCov_cov_y_zmsgVelEcefCov_cov_z_zmsgVelEcefCov_flagsmsgVelEcefCov_n_satsmsgVelEcefCov_towmsgVelEcefCov_xmsgVelEcefCov_ymsgVelEcefCov_z msgVelNed$fBinaryMsgVelNed$fShowMsgVelNed$fReadMsgVelNed $fEqMsgVelNed$fToSBPMsgVelNed$fFromJSONMsgVelNed$fToJSONMsgVelNed MsgVelNedCov_msgVelNedCov_tow_msgVelNedCov_n_msgVelNedCov_e_msgVelNedCov_d_msgVelNedCov_cov_n_n_msgVelNedCov_cov_n_e_msgVelNedCov_cov_n_d_msgVelNedCov_cov_e_e_msgVelNedCov_cov_e_d_msgVelNedCov_cov_d_d_msgVelNedCov_n_sats_msgVelNedCov_flags msgVelNed_d msgVelNed_emsgVelNed_flagsmsgVelNed_h_accuracy msgVelNed_nmsgVelNed_n_sats msgVelNed_towmsgVelNed_v_accuracy msgVelNedCov$fBinaryMsgVelNedCov$fShowMsgVelNedCov$fReadMsgVelNedCov$fEqMsgVelNedCov$fToSBPMsgVelNedCov$fFromJSONMsgVelNedCov$fToJSONMsgVelNedCov MsgVelBody_msgVelBody_tow _msgVelBody_x _msgVelBody_y 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msgInitBase$fBinaryMsgInitBase$fShowMsgInitBase$fReadMsgInitBase$fEqMsgInitBase$fToSBPMsgInitBase$fFromJSONMsgInitBase$fToJSONMsgInitBaseMsgThreadState_msgThreadState_name_msgThreadState_cpu_msgThreadState_stack_freemsgThreadState$fBinaryMsgThreadState$fShowMsgThreadState$fReadMsgThreadState$fEqMsgThreadState$fToSBPMsgThreadState$fFromJSONMsgThreadState$fToJSONMsgThreadState UARTChannel_uARTChannel_tx_throughput_uARTChannel_rx_throughput_uARTChannel_crc_error_count_uARTChannel_io_error_count_uARTChannel_tx_buffer_level_uARTChannel_rx_buffer_levelmsgThreadState_cpumsgThreadState_namemsgThreadState_stack_free$fBinaryUARTChannel$fShowUARTChannel$fReadUARTChannel$fEqUARTChannel$fFromJSONUARTChannel$fToJSONUARTChannelPeriod _period_avg _period_pmin _period_pmax_period_currentuARTChannel_crc_error_countuARTChannel_io_error_countuARTChannel_rx_buffer_leveluARTChannel_rx_throughputuARTChannel_tx_buffer_leveluARTChannel_tx_throughput$fBinaryPeriod $fShowPeriod $fReadPeriod $fEqPeriod$fFromJSONPeriod$fToJSONPeriodLatency _latency_avg _latency_lmin _latency_lmax_latency_current period_avgperiod_current period_pmax period_pmin$fBinaryLatency $fShowLatency $fReadLatency $fEqLatency$fFromJSONLatency$fToJSONLatency MsgUartState_msgUartState_uart_a_msgUartState_uart_b_msgUartState_uart_ftdi_msgUartState_latency_msgUartState_obs_period latency_avglatency_current latency_lmax latency_lmin msgUartState$fBinaryMsgUartState$fShowMsgUartState$fReadMsgUartState$fEqMsgUartState$fToSBPMsgUartState$fFromJSONMsgUartState$fToJSONMsgUartStateMsgUartStateDepa_msgUartStateDepa_uart_a_msgUartStateDepa_uart_b_msgUartStateDepa_uart_ftdi_msgUartStateDepa_latencymsgUartState_latencymsgUartState_obs_periodmsgUartState_uart_amsgUartState_uart_bmsgUartState_uart_ftdimsgUartStateDepa$fBinaryMsgUartStateDepa$fShowMsgUartStateDepa$fReadMsgUartStateDepa$fEqMsgUartStateDepa$fToSBPMsgUartStateDepa$fFromJSONMsgUartStateDepa$fToJSONMsgUartStateDepa MsgIarState_msgIarState_num_hypsmsgUartStateDepa_latencymsgUartStateDepa_uart_amsgUartStateDepa_uart_bmsgUartStateDepa_uart_ftdi msgIarState$fBinaryMsgIarState$fShowMsgIarState$fReadMsgIarState$fEqMsgIarState$fToSBPMsgIarState$fFromJSONMsgIarState$fToJSONMsgIarStateMsgMaskSatellite_msgMaskSatellite_mask_msgMaskSatellite_sidmsgIarState_num_hypsmsgMaskSatellite$fBinaryMsgMaskSatellite$fShowMsgMaskSatellite$fReadMsgMaskSatellite$fEqMsgMaskSatellite$fToSBPMsgMaskSatellite$fFromJSONMsgMaskSatellite$fToJSONMsgMaskSatelliteMsgMaskSatelliteDep_msgMaskSatelliteDep_mask_msgMaskSatelliteDep_sidmsgMaskSatellite_maskmsgMaskSatellite_sidmsgMaskSatelliteDep$fBinaryMsgMaskSatelliteDep$fShowMsgMaskSatelliteDep$fReadMsgMaskSatelliteDep$fEqMsgMaskSatelliteDep$fToSBPMsgMaskSatelliteDep$fFromJSONMsgMaskSatelliteDep$fToJSONMsgMaskSatelliteDepMsgDeviceMonitor_msgDeviceMonitor_dev_vin_msgDeviceMonitor_cpu_vint_msgDeviceMonitor_cpu_vaux!_msgDeviceMonitor_cpu_temperature _msgDeviceMonitor_fe_temperaturemsgMaskSatelliteDep_maskmsgMaskSatelliteDep_sidmsgDeviceMonitor$fBinaryMsgDeviceMonitor$fShowMsgDeviceMonitor$fReadMsgDeviceMonitor$fEqMsgDeviceMonitor$fToSBPMsgDeviceMonitor$fFromJSONMsgDeviceMonitor$fToJSONMsgDeviceMonitor MsgCommandReq_msgCommandReq_sequence_msgCommandReq_command msgDeviceMonitor_cpu_temperaturemsgDeviceMonitor_cpu_vauxmsgDeviceMonitor_cpu_vintmsgDeviceMonitor_dev_vinmsgDeviceMonitor_fe_temperature msgCommandReq$fBinaryMsgCommandReq$fShowMsgCommandReq$fReadMsgCommandReq$fEqMsgCommandReq$fToSBPMsgCommandReq$fFromJSONMsgCommandReq$fToJSONMsgCommandReqMsgCommandResp_msgCommandResp_sequence_msgCommandResp_codemsgCommandReq_commandmsgCommandReq_sequencemsgCommandResp$fBinaryMsgCommandResp$fShowMsgCommandResp$fReadMsgCommandResp$fEqMsgCommandResp$fToSBPMsgCommandResp$fFromJSONMsgCommandResp$fToJSONMsgCommandRespMsgCommandOutput_msgCommandOutput_sequence_msgCommandOutput_linemsgCommandResp_codemsgCommandResp_sequencemsgCommandOutput$fBinaryMsgCommandOutput$fShowMsgCommandOutput$fReadMsgCommandOutput$fEqMsgCommandOutput$fToSBPMsgCommandOutput$fFromJSONMsgCommandOutput$fToJSONMsgCommandOutputMsgNetworkStateReqmsgCommandOutput_linemsgCommandOutput_sequencemsgNetworkStateReq$fBinaryMsgNetworkStateReq$fShowMsgNetworkStateReq$fReadMsgNetworkStateReq$fEqMsgNetworkStateReq$fToSBPMsgNetworkStateReq$fFromJSONMsgNetworkStateReq$fToJSONMsgNetworkStateReqMsgNetworkStateResp!_msgNetworkStateResp_ipv4_address#_msgNetworkStateResp_ipv4_mask_size!_msgNetworkStateResp_ipv6_address#_msgNetworkStateResp_ipv6_mask_size_msgNetworkStateResp_rx_bytes_msgNetworkStateResp_tx_bytes#_msgNetworkStateResp_interface_name_msgNetworkStateResp_flagsmsgNetworkStateResp$fBinaryMsgNetworkStateResp$fShowMsgNetworkStateResp$fReadMsgNetworkStateResp$fEqMsgNetworkStateResp$fToSBPMsgNetworkStateResp$fFromJSONMsgNetworkStateResp$fToJSONMsgNetworkStateResp NetworkUsage_networkUsage_duration_networkUsage_total_bytes_networkUsage_rx_bytes_networkUsage_tx_bytes_networkUsage_interface_namemsgNetworkStateResp_flags"msgNetworkStateResp_interface_name msgNetworkStateResp_ipv4_address"msgNetworkStateResp_ipv4_mask_size msgNetworkStateResp_ipv6_address"msgNetworkStateResp_ipv6_mask_sizemsgNetworkStateResp_rx_bytesmsgNetworkStateResp_tx_bytes$fBinaryNetworkUsage$fShowNetworkUsage$fReadNetworkUsage$fEqNetworkUsage$fFromJSONNetworkUsage$fToJSONNetworkUsageMsgNetworkBandwidthUsage$_msgNetworkBandwidthUsage_interfacesnetworkUsage_durationnetworkUsage_interface_namenetworkUsage_rx_bytesnetworkUsage_total_bytesnetworkUsage_tx_bytesmsgNetworkBandwidthUsage $fBinaryMsgNetworkBandwidthUsage$fShowMsgNetworkBandwidthUsage$fReadMsgNetworkBandwidthUsage$fEqMsgNetworkBandwidthUsage$fToSBPMsgNetworkBandwidthUsage"$fFromJSONMsgNetworkBandwidthUsage $fToJSONMsgNetworkBandwidthUsageMsgCellModemStatus#_msgCellModemStatus_signal_strength%_msgCellModemStatus_signal_error_rate_msgCellModemStatus_reserved#msgNetworkBandwidthUsage_interfacesmsgCellModemStatus$fBinaryMsgCellModemStatus$fShowMsgCellModemStatus$fReadMsgCellModemStatus$fEqMsgCellModemStatus$fToSBPMsgCellModemStatus$fFromJSONMsgCellModemStatus$fToJSONMsgCellModemStatus MsgSpecanDep_msgSpecanDep_channel_tag_msgSpecanDep_t_msgSpecanDep_freq_ref_msgSpecanDep_freq_step_msgSpecanDep_amplitude_ref_msgSpecanDep_amplitude_unit_msgSpecanDep_amplitude_valuemsgCellModemStatus_reserved$msgCellModemStatus_signal_error_rate"msgCellModemStatus_signal_strength msgSpecanDep$fBinaryMsgSpecanDep$fShowMsgSpecanDep$fReadMsgSpecanDep$fEqMsgSpecanDep$fToSBPMsgSpecanDep$fFromJSONMsgSpecanDep$fToJSONMsgSpecanDep MsgSpecan_msgSpecan_channel_tag _msgSpecan_t_msgSpecan_freq_ref_msgSpecan_freq_step_msgSpecan_amplitude_ref_msgSpecan_amplitude_unit_msgSpecan_amplitude_valuemsgSpecanDep_amplitude_refmsgSpecanDep_amplitude_unitmsgSpecanDep_amplitude_valuemsgSpecanDep_channel_tagmsgSpecanDep_freq_refmsgSpecanDep_freq_stepmsgSpecanDep_t msgSpecan$fBinaryMsgSpecan$fShowMsgSpecan$fReadMsgSpecan $fEqMsgSpecan$fToSBPMsgSpecan$fFromJSONMsgSpecan$fToJSONMsgSpecanmsgSpecan_amplitude_refmsgSpecan_amplitude_unitmsgSpecan_amplitude_valuemsgSpecan_channel_tagmsgSpecan_freq_refmsgSpecan_freq_step msgSpecan_tObservationHeader_observationHeader_t_observationHeader_n_obs$fBinaryObservationHeader$fShowObservationHeader$fReadObservationHeader$fEqObservationHeader$fFromJSONObservationHeader$fToJSONObservationHeaderDoppler _doppler_i _doppler_fobservationHeader_n_obsobservationHeader_t$fBinaryDoppler $fShowDoppler $fReadDoppler $fEqDoppler$fFromJSONDoppler$fToJSONDopplerPackedObsContent_packedObsContent_P_packedObsContent_L_packedObsContent_D_packedObsContent_cn0_packedObsContent_lock_packedObsContent_flags_packedObsContent_sid doppler_f doppler_i$fBinaryPackedObsContent$fShowPackedObsContent$fReadPackedObsContent$fEqPackedObsContent$fFromJSONPackedObsContent$fToJSONPackedObsContentMsgObs_msgObs_header _msgObs_obspackedObsContent_DpackedObsContent_LpackedObsContent_PpackedObsContent_cn0packedObsContent_flagspackedObsContent_lockpackedObsContent_sidmsgObs$fBinaryMsgObs $fShowMsgObs $fReadMsgObs $fEqMsgObs $fToSBPMsgObs$fFromJSONMsgObs$fToJSONMsgObs MsgBasePosLlh_msgBasePosLlh_lat_msgBasePosLlh_lon_msgBasePosLlh_height msgObs_header msgObs_obs msgBasePosLlh$fBinaryMsgBasePosLlh$fShowMsgBasePosLlh$fReadMsgBasePosLlh$fEqMsgBasePosLlh$fToSBPMsgBasePosLlh$fFromJSONMsgBasePosLlh$fToJSONMsgBasePosLlhMsgBasePosEcef_msgBasePosEcef_x_msgBasePosEcef_y_msgBasePosEcef_zmsgBasePosLlh_heightmsgBasePosLlh_latmsgBasePosLlh_lonmsgBasePosEcef$fBinaryMsgBasePosEcef$fShowMsgBasePosEcef$fReadMsgBasePosEcef$fEqMsgBasePosEcef$fToSBPMsgBasePosEcef$fFromJSONMsgBasePosEcef$fToJSONMsgBasePosEcefEphemerisCommonContent_ephemerisCommonContent_sid_ephemerisCommonContent_toe_ephemerisCommonContent_ura$_ephemerisCommonContent_fit_interval_ephemerisCommonContent_valid#_ephemerisCommonContent_health_bitsmsgBasePosEcef_xmsgBasePosEcef_ymsgBasePosEcef_z$fBinaryEphemerisCommonContent$fShowEphemerisCommonContent$fReadEphemerisCommonContent$fEqEphemerisCommonContent $fFromJSONEphemerisCommonContent$fToJSONEphemerisCommonContentEphemerisCommonContentDepA_ephemerisCommonContentDepA_sid_ephemerisCommonContentDepA_toe_ephemerisCommonContentDepA_ura(_ephemerisCommonContentDepA_fit_interval!_ephemerisCommonContentDepA_valid'_ephemerisCommonContentDepA_health_bits#ephemerisCommonContent_fit_interval"ephemerisCommonContent_health_bitsephemerisCommonContent_sidephemerisCommonContent_toeephemerisCommonContent_uraephemerisCommonContent_valid"$fBinaryEphemerisCommonContentDepA $fShowEphemerisCommonContentDepA 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