Commit 924c475d authored by PX4BuildBot's avatar PX4BuildBot

autogenerated headers for rev...

autogenerated headers for rev https://github.com/mavlink/mavlink/tree/491c5ee4a1345ef6deb2173fc2468ddf783fb6d5
parent 59143261
......@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed May 16 2018"
#define MAVLINK_BUILD_DATE "Fri May 18 2018"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
......
......@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed May 16 2018"
#define MAVLINK_BUILD_DATE "Fri May 18 2018"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
......
......@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed May 16 2018"
#define MAVLINK_BUILD_DATE "Fri May 18 2018"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
......
......@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed May 16 2018"
#define MAVLINK_BUILD_DATE "Fri May 18 2018"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
......
......@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed May 16 2018"
#define MAVLINK_BUILD_DATE "Fri May 18 2018"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
......
......@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed May 16 2018"
#define MAVLINK_BUILD_DATE "Fri May 18 2018"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
......
......@@ -133,16 +133,16 @@
<description>Sensor and DSC control loads.</description>
<field name="sensLoad" type="uint8_t">Sensor DSC Load</field>
<field name="ctrlLoad" type="uint8_t">Control DSC Load</field>
<field name="batVolt" type="uint16_t">Battery Voltage in millivolts</field>
<field name="batVolt" type="uint16_t" units="mV">Battery Voltage</field>
</message>
<message name="SENSOR_BIAS" id="172">
<description>Accelerometer and gyro biases.</description>
<field name="axBias" type="float">Accelerometer X bias (m/s)</field>
<field name="ayBias" type="float">Accelerometer Y bias (m/s)</field>
<field name="azBias" type="float">Accelerometer Z bias (m/s)</field>
<field name="gxBias" type="float">Gyro X bias (rad/s)</field>
<field name="gyBias" type="float">Gyro Y bias (rad/s)</field>
<field name="gzBias" type="float">Gyro Z bias (rad/s)</field>
<field name="axBias" type="float" units="m/s">Accelerometer X bias</field>
<field name="ayBias" type="float" units="m/s">Accelerometer Y bias</field>
<field name="azBias" type="float" units="m/s">Accelerometer Z bias</field>
<field name="gxBias" type="float" units="rad/s">Gyro X bias</field>
<field name="gyBias" type="float" units="rad/s">Gyro Y bias</field>
<field name="gzBias" type="float" units="rad/s">Gyro Z bias</field>
</message>
<message name="DIAGNOSTIC" id="173">
<description>Configurable diagnostic messages.</description>
......@@ -155,7 +155,7 @@
</message>
<message name="SLUGS_NAVIGATION" id="176">
<description>Data used in the navigation algorithm.</description>
<field name="u_m" type="float">Measured Airspeed prior to the nav filter in m/s</field>
<field name="u_m" type="float" units="m/s">Measured Airspeed prior to the nav filter</field>
<field name="phi_c" type="float">Commanded Roll</field>
<field name="theta_c" type="float">Commanded Pitch</field>
<field name="psiDot_c" type="float">Commanded Turn rate</field>
......@@ -164,7 +164,7 @@
<field name="dist2Go" type="float">Remaining distance to Run on this leg of Navigation</field>
<field name="fromWP" type="uint8_t">Origin WP</field>
<field name="toWP" type="uint8_t">Destination WP</field>
<field name="h_c" type="uint16_t">Commanded altitude in 0.1 m</field>
<field name="h_c" type="uint16_t" units="dm">Commanded altitude</field>
</message>
<message name="DATA_LOG" id="177">
<description>Configurable data log probes to be used inside Simulink</description>
......@@ -188,19 +188,19 @@
<field name="useSat" type="uint8_t">Used satellites in Solution </field>
<field name="GppGl" type="uint8_t">GPS+GLONASS satellites in Solution </field>
<field name="sigUsedMask" type="uint8_t">GPS and GLONASS usage mask (bit 0 GPS_used? bit_4 GLONASS_used?)</field>
<field name="percentUsed" type="uint8_t">Percent used GPS</field>
<field name="percentUsed" type="uint8_t" units="%">Percent used GPS</field>
</message>
<message name="MID_LVL_CMDS" id="180">
<description>Mid Level commands sent from the GS to the autopilot. These are only sent when being operated in mid-level commands mode from the ground.</description>
<field name="target" type="uint8_t">The system setting the commands</field>
<field name="hCommand" type="float">Commanded Altitude in meters</field>
<field name="uCommand" type="float">Commanded Airspeed in m/s</field>
<field name="rCommand" type="float">Commanded Turnrate in rad/s</field>
<field name="hCommand" type="float" units="m">Commanded Altitude</field>
<field name="uCommand" type="float" units="m/s">Commanded Airspeed</field>
<field name="rCommand" type="float" units="rad/s">Commanded Turnrate</field>
</message>
<message name="CTRL_SRFC_PT" id="181">
<description>This message sets the control surfaces for selective passthrough mode.</description>
<field name="target" type="uint8_t">The system setting the commands</field>
<field name="bitfieldPt" type="uint16_t">Bitfield containing the passthrough configuration, see CONTROL_SURFACE_FLAG ENUM.</field>
<field name="bitfieldPt" type="uint16_t" enum="CONTROL_SURFACE_FLAG" display="bitmask">Bitfield containing the passthrough configuration, see CONTROL_SURFACE_FLAG ENUM.</field>
</message>
<message name="SLUGS_CAMERA_ORDER" id="184">
<description>Orders generated to the SLUGS camera mount. </description>
......@@ -229,8 +229,8 @@
<message name="SLUGS_MOBILE_LOCATION" id="186">
<description>Transmits the last known position of the mobile GS to the UAV. Very relevant when Track Mobile is enabled</description>
<field name="target" type="uint8_t">The system reporting the action</field>
<field name="latitude" type="float">Mobile Latitude</field>
<field name="longitude" type="float">Mobile Longitude</field>
<field name="latitude" type="float" units="deg">Mobile Latitude</field>
<field name="longitude" type="float" units="deg">Mobile Longitude</field>
</message>
<message name="SLUGS_CONFIGURATION_CAMERA" id="188">
<description>Control for camara.</description>
......@@ -241,8 +241,8 @@
<message name="ISR_LOCATION" id="189">
<description>Transmits the position of watch</description>
<field name="target" type="uint8_t">The system reporting the action</field>
<field name="latitude" type="float">ISR Latitude</field>
<field name="longitude" type="float">ISR Longitude</field>
<field name="latitude" type="float" units="deg">ISR Latitude</field>
<field name="longitude" type="float" units="deg">ISR Longitude</field>
<field name="height" type="float">ISR Height</field>
<field name="option1" type="uint8_t">Option 1</field>
<field name="option2" type="uint8_t">Option 2</field>
......@@ -272,10 +272,10 @@
<message name="UAV_STATUS" id="193">
<description>Transmits the actual status values UAV in flight</description>
<field name="target" type="uint8_t">The ID system reporting the action</field>
<field name="latitude" type="float">Latitude UAV</field>
<field name="longitude" type="float">Longitude UAV</field>
<field name="altitude" type="float">Altitude UAV</field>
<field name="speed" type="float">Speed UAV</field>
<field name="latitude" type="float" units="deg">Latitude UAV</field>
<field name="longitude" type="float" units="deg">Longitude UAV</field>
<field name="altitude" type="float" units="m">Altitude UAV</field>
<field name="speed" type="float" units="m/s">Speed UAV</field>
<field name="course" type="float">Course UAV</field>
</message>
<message name="STATUS_GPS" id="194">
......@@ -284,7 +284,7 @@
<field name="gpsQuality" type="uint8_t">The quality indicator, 0=fix not available or invalid, 1=GPS fix, 2=C/A differential GPS, 6=Dead reckoning mode, 7=Manual input mode (fixed position), 8=Simulator mode, 9= WAAS a</field>
<field name="msgsType" type="uint8_t"> Indicates if GN, GL or GP messages are being received</field>
<field name="posStatus" type="uint8_t"> A = data valid, V = data invalid</field>
<field name="magVar" type="float">Magnetic variation, degrees </field>
<field name="magVar" type="float" units="deg">Magnetic variation</field>
<field name="magDir" type="int8_t"> Magnetic variation direction E/W. Easterly variation (E) subtracts from True course and Westerly variation (W) adds to True course</field>
<field name="modeInd" type="uint8_t"> Positioning system mode indicator. A - Autonomous;D-Differential; E-Estimated (dead reckoning) mode;M-Manual input; N-Data not valid</field>
</message>
......@@ -295,7 +295,7 @@
<field name="solStatus" type="uint8_t">solution Status. See table 44 page 197</field>
<field name="posType" type="uint8_t">position type. See table 43 page 196</field>
<field name="velType" type="uint8_t">velocity type. See table 43 page 196</field>
<field name="posSolAge" type="float">Age of the position solution in seconds</field>
<field name="posSolAge" type="float" units="s">Age of the position solution</field>
<field name="csFails" type="uint16_t">Times the CRC has failed since boot</field>
</message>
<message name="SENSOR_DIAG" id="196">
......
......@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed May 16 2018"
#define MAVLINK_BUILD_DATE "Fri May 18 2018"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 9
......
......@@ -5,7 +5,7 @@
MAVPACKED(
typedef struct __mavlink_cpu_load_t {
uint16_t batVolt; /*< Battery Voltage in millivolts*/
uint16_t batVolt; /*< Battery Voltage*/
uint8_t sensLoad; /*< Sensor DSC Load*/
uint8_t ctrlLoad; /*< Control DSC Load*/
}) mavlink_cpu_load_t;
......@@ -49,7 +49,7 @@ typedef struct __mavlink_cpu_load_t {
*
* @param sensLoad Sensor DSC Load
* @param ctrlLoad Control DSC Load
* @param batVolt Battery Voltage in millivolts
* @param batVolt Battery Voltage
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_cpu_load_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
......@@ -83,7 +83,7 @@ static inline uint16_t mavlink_msg_cpu_load_pack(uint8_t system_id, uint8_t comp
* @param msg The MAVLink message to compress the data into
* @param sensLoad Sensor DSC Load
* @param ctrlLoad Control DSC Load
* @param batVolt Battery Voltage in millivolts
* @param batVolt Battery Voltage
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_cpu_load_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
......@@ -143,7 +143,7 @@ static inline uint16_t mavlink_msg_cpu_load_encode_chan(uint8_t system_id, uint8
*
* @param sensLoad Sensor DSC Load
* @param ctrlLoad Control DSC Load
* @param batVolt Battery Voltage in millivolts
* @param batVolt Battery Voltage
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
......@@ -236,7 +236,7 @@ static inline uint8_t mavlink_msg_cpu_load_get_ctrlLoad(const mavlink_message_t*
/**
* @brief Get field batVolt from cpu_load message
*
* @return Battery Voltage in millivolts
* @return Battery Voltage
*/
static inline uint16_t mavlink_msg_cpu_load_get_batVolt(const mavlink_message_t* msg)
{
......
......@@ -5,9 +5,9 @@
MAVPACKED(
typedef struct __mavlink_mid_lvl_cmds_t {
float hCommand; /*< Commanded Altitude in meters*/
float uCommand; /*< Commanded Airspeed in m/s*/
float rCommand; /*< Commanded Turnrate in rad/s*/
float hCommand; /*< Commanded Altitude*/
float uCommand; /*< Commanded Airspeed*/
float rCommand; /*< Commanded Turnrate*/
uint8_t target; /*< The system setting the commands*/
}) mavlink_mid_lvl_cmds_t;
......@@ -51,9 +51,9 @@ typedef struct __mavlink_mid_lvl_cmds_t {
* @param msg The MAVLink message to compress the data into
*
* @param target The system setting the commands
* @param hCommand Commanded Altitude in meters
* @param uCommand Commanded Airspeed in m/s
* @param rCommand Commanded Turnrate in rad/s
* @param hCommand Commanded Altitude
* @param uCommand Commanded Airspeed
* @param rCommand Commanded Turnrate
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_mid_lvl_cmds_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
......@@ -88,9 +88,9 @@ static inline uint16_t mavlink_msg_mid_lvl_cmds_pack(uint8_t system_id, uint8_t
* @param chan The MAVLink channel this message will be sent over
* @param msg The MAVLink message to compress the data into
* @param target The system setting the commands
* @param hCommand Commanded Altitude in meters
* @param uCommand Commanded Airspeed in m/s
* @param rCommand Commanded Turnrate in rad/s
* @param hCommand Commanded Altitude
* @param uCommand Commanded Airspeed
* @param rCommand Commanded Turnrate
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_mid_lvl_cmds_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
......@@ -151,9 +151,9 @@ static inline uint16_t mavlink_msg_mid_lvl_cmds_encode_chan(uint8_t system_id, u
* @param chan MAVLink channel to send the message
*
* @param target The system setting the commands
* @param hCommand Commanded Altitude in meters
* @param uCommand Commanded Airspeed in m/s
* @param rCommand Commanded Turnrate in rad/s
* @param hCommand Commanded Altitude
* @param uCommand Commanded Airspeed
* @param rCommand Commanded Turnrate
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
......@@ -240,7 +240,7 @@ static inline uint8_t mavlink_msg_mid_lvl_cmds_get_target(const mavlink_message_
/**
* @brief Get field hCommand from mid_lvl_cmds message
*
* @return Commanded Altitude in meters
* @return Commanded Altitude
*/
static inline float mavlink_msg_mid_lvl_cmds_get_hCommand(const mavlink_message_t* msg)
{
......@@ -250,7 +250,7 @@ static inline float mavlink_msg_mid_lvl_cmds_get_hCommand(const mavlink_message_
/**
* @brief Get field uCommand from mid_lvl_cmds message
*
* @return Commanded Airspeed in m/s
* @return Commanded Airspeed
*/
static inline float mavlink_msg_mid_lvl_cmds_get_uCommand(const mavlink_message_t* msg)
{
......@@ -260,7 +260,7 @@ static inline float mavlink_msg_mid_lvl_cmds_get_uCommand(const mavlink_message_
/**
* @brief Get field rCommand from mid_lvl_cmds message
*
* @return Commanded Turnrate in rad/s
* @return Commanded Turnrate
*/
static inline float mavlink_msg_mid_lvl_cmds_get_rCommand(const mavlink_message_t* msg)
{
......
......@@ -6,7 +6,7 @@
MAVPACKED(
typedef struct __mavlink_novatel_diag_t {
uint32_t receiverStatus; /*< Status Bitfield. See table 69 page 350 Novatel OEMstar Manual*/
float posSolAge; /*< Age of the position solution in seconds*/
float posSolAge; /*< Age of the position solution*/
uint16_t csFails; /*< Times the CRC has failed since boot*/
uint8_t timeStatus; /*< The Time Status. See Table 8 page 27 Novatel OEMStar Manual*/
uint8_t solStatus; /*< solution Status. See table 44 page 197*/
......@@ -64,7 +64,7 @@ typedef struct __mavlink_novatel_diag_t {
* @param solStatus solution Status. See table 44 page 197
* @param posType position type. See table 43 page 196
* @param velType velocity type. See table 43 page 196
* @param posSolAge Age of the position solution in seconds
* @param posSolAge Age of the position solution
* @param csFails Times the CRC has failed since boot
* @return length of the message in bytes (excluding serial stream start sign)
*/
......@@ -110,7 +110,7 @@ static inline uint16_t mavlink_msg_novatel_diag_pack(uint8_t system_id, uint8_t
* @param solStatus solution Status. See table 44 page 197
* @param posType position type. See table 43 page 196
* @param velType velocity type. See table 43 page 196
* @param posSolAge Age of the position solution in seconds
* @param posSolAge Age of the position solution
* @param csFails Times the CRC has failed since boot
* @return length of the message in bytes (excluding serial stream start sign)
*/
......@@ -182,7 +182,7 @@ static inline uint16_t mavlink_msg_novatel_diag_encode_chan(uint8_t system_id, u
* @param solStatus solution Status. See table 44 page 197
* @param posType position type. See table 43 page 196
* @param velType velocity type. See table 43 page 196
* @param posSolAge Age of the position solution in seconds
* @param posSolAge Age of the position solution
* @param csFails Times the CRC has failed since boot
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
......@@ -322,7 +322,7 @@ static inline uint8_t mavlink_msg_novatel_diag_get_velType(const mavlink_message
/**
* @brief Get field posSolAge from novatel_diag message
*
* @return Age of the position solution in seconds
* @return Age of the position solution
*/
static inline float mavlink_msg_novatel_diag_get_posSolAge(const mavlink_message_t* msg)
{
......
......@@ -5,12 +5,12 @@
MAVPACKED(
typedef struct __mavlink_sensor_bias_t {
float axBias; /*< Accelerometer X bias (m/s)*/
float ayBias; /*< Accelerometer Y bias (m/s)*/
float azBias; /*< Accelerometer Z bias (m/s)*/
float gxBias; /*< Gyro X bias (rad/s)*/
float gyBias; /*< Gyro Y bias (rad/s)*/
float gzBias; /*< Gyro Z bias (rad/s)*/
float axBias; /*< Accelerometer X bias*/
float ayBias; /*< Accelerometer Y bias*/
float azBias; /*< Accelerometer Z bias*/
float gxBias; /*< Gyro X bias*/
float gyBias; /*< Gyro Y bias*/
float gzBias; /*< Gyro Z bias*/
}) mavlink_sensor_bias_t;
#define MAVLINK_MSG_ID_SENSOR_BIAS_LEN 24
......@@ -56,12 +56,12 @@ typedef struct __mavlink_sensor_bias_t {
* @param component_id ID of this component (e.g. 200 for IMU)
* @param msg The MAVLink message to compress the data into
*
* @param axBias Accelerometer X bias (m/s)
* @param ayBias Accelerometer Y bias (m/s)
* @param azBias Accelerometer Z bias (m/s)
* @param gxBias Gyro X bias (rad/s)
* @param gyBias Gyro Y bias (rad/s)
* @param gzBias Gyro Z bias (rad/s)
* @param axBias Accelerometer X bias
* @param ayBias Accelerometer Y bias
* @param azBias Accelerometer Z bias
* @param gxBias Gyro X bias
* @param gyBias Gyro Y bias
* @param gzBias Gyro Z bias
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_sensor_bias_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
......@@ -99,12 +99,12 @@ static inline uint16_t mavlink_msg_sensor_bias_pack(uint8_t system_id, uint8_t c
* @param component_id ID of this component (e.g. 200 for IMU)
* @param chan The MAVLink channel this message will be sent over
* @param msg The MAVLink message to compress the data into
* @param axBias Accelerometer X bias (m/s)
* @param ayBias Accelerometer Y bias (m/s)
* @param azBias Accelerometer Z bias (m/s)
* @param gxBias Gyro X bias (rad/s)
* @param gyBias Gyro Y bias (rad/s)
* @param gzBias Gyro Z bias (rad/s)
* @param axBias Accelerometer X bias
* @param ayBias Accelerometer Y bias
* @param azBias Accelerometer Z bias
* @param gxBias Gyro X bias
* @param gyBias Gyro Y bias
* @param gzBias Gyro Z bias
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_sensor_bias_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
......@@ -168,12 +168,12 @@ static inline uint16_t mavlink_msg_sensor_bias_encode_chan(uint8_t system_id, ui
* @brief Send a sensor_bias message
* @param chan MAVLink channel to send the message
*
* @param axBias Accelerometer X bias (m/s)
* @param ayBias Accelerometer Y bias (m/s)
* @param azBias Accelerometer Z bias (m/s)
* @param gxBias Gyro X bias (rad/s)
* @param gyBias Gyro Y bias (rad/s)
* @param gzBias Gyro Z bias (rad/s)
* @param axBias Accelerometer X bias
* @param ayBias Accelerometer Y bias
* @param azBias Accelerometer Z bias
* @param gxBias Gyro X bias
* @param gyBias Gyro Y bias
* @param gzBias Gyro Z bias
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
......@@ -258,7 +258,7 @@ static inline void mavlink_msg_sensor_bias_send_buf(mavlink_message_t *msgbuf, m
/**
* @brief Get field axBias from sensor_bias message
*
* @return Accelerometer X bias (m/s)
* @return Accelerometer X bias
*/
static inline float mavlink_msg_sensor_bias_get_axBias(const mavlink_message_t* msg)
{
......@@ -268,7 +268,7 @@ static inline float mavlink_msg_sensor_bias_get_axBias(const mavlink_message_t*
/**
* @brief Get field ayBias from sensor_bias message
*
* @return Accelerometer Y bias (m/s)
* @return Accelerometer Y bias
*/
static inline float mavlink_msg_sensor_bias_get_ayBias(const mavlink_message_t* msg)
{
......@@ -278,7 +278,7 @@ static inline float mavlink_msg_sensor_bias_get_ayBias(const mavlink_message_t*
/**
* @brief Get field azBias from sensor_bias message
*
* @return Accelerometer Z bias (m/s)
* @return Accelerometer Z bias
*/
static inline float mavlink_msg_sensor_bias_get_azBias(const mavlink_message_t* msg)
{
......@@ -288,7 +288,7 @@ static inline float mavlink_msg_sensor_bias_get_azBias(const mavlink_message_t*
/**
* @brief Get field gxBias from sensor_bias message
*
* @return Gyro X bias (rad/s)
* @return Gyro X bias
*/
static inline float mavlink_msg_sensor_bias_get_gxBias(const mavlink_message_t* msg)
{
......@@ -298,7 +298,7 @@ static inline float mavlink_msg_sensor_bias_get_gxBias(const mavlink_message_t*
/**
* @brief Get field gyBias from sensor_bias message
*
* @return Gyro Y bias (rad/s)
* @return Gyro Y bias
*/
static inline float mavlink_msg_sensor_bias_get_gyBias(const mavlink_message_t* msg)
{
......@@ -308,7 +308,7 @@ static inline float mavlink_msg_sensor_bias_get_gyBias(const mavlink_message_t*
/**
* @brief Get field gzBias from sensor_bias message
*
* @return Gyro Z bias (rad/s)
* @return Gyro Z bias
*/
static inline float mavlink_msg_sensor_bias_get_gzBias(const mavlink_message_t* msg)
{
......
......@@ -5,14 +5,14 @@
MAVPACKED(
typedef struct __mavlink_slugs_navigation_t {
float u_m; /*< Measured Airspeed prior to the nav filter in m/s*/
float u_m; /*< Measured Airspeed prior to the nav filter*/
float phi_c; /*< Commanded Roll*/
float theta_c; /*< Commanded Pitch*/
float psiDot_c; /*< Commanded Turn rate*/
float ay_body; /*< Y component of the body acceleration*/
float totalDist; /*< Total Distance to Run on this leg of Navigation*/
float dist2Go; /*< Remaining distance to Run on this leg of Navigation*/
uint16_t h_c; /*< Commanded altitude in 0.1 m*/
uint16_t h_c; /*< Commanded altitude*/
uint8_t fromWP; /*< Origin WP*/
uint8_t toWP; /*< Destination WP*/
}) mavlink_slugs_navigation_t;
......@@ -68,7 +68,7 @@ typedef struct __mavlink_slugs_navigation_t {
* @param component_id ID of this component (e.g. 200 for IMU)
* @param msg The MAVLink message to compress the data into
*
* @param u_m Measured Airspeed prior to the nav filter in m/s
* @param u_m Measured Airspeed prior to the nav filter
* @param phi_c Commanded Roll
* @param theta_c Commanded Pitch
* @param psiDot_c Commanded Turn rate
......@@ -77,7 +77,7 @@ typedef struct __mavlink_slugs_navigation_t {
* @param dist2Go Remaining distance to Run on this leg of Navigation
* @param fromWP Origin WP
* @param toWP Destination WP
* @param h_c Commanded altitude in 0.1 m
* @param h_c Commanded altitude
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_slugs_navigation_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
......@@ -123,7 +123,7 @@ static inline uint16_t mavlink_msg_slugs_navigation_pack(uint8_t system_id, uint
* @param component_id ID of this component (e.g. 200 for IMU)
* @param chan The MAVLink channel this message will be sent over
* @param msg The MAVLink message to compress the data into
* @param u_m Measured Airspeed prior to the nav filter in m/s
* @param u_m Measured Airspeed prior to the nav filter
* @param phi_c Commanded Roll
* @param theta_c Commanded Pitch
* @param psiDot_c Commanded Turn rate
......@@ -132,7 +132,7 @@ static inline uint16_t mavlink_msg_slugs_navigation_pack(uint8_t system_id, uint
* @param dist2Go Remaining distance to Run on this leg of Navigation
* @param fromWP Origin WP
* @param toWP Destination WP
* @param h_c Commanded altitude in 0.1 m
* @param h_c Commanded altitude
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_slugs_navigation_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
......@@ -204,7 +204,7 @@ static inline uint16_t mavlink_msg_slugs_navigation_encode_chan(uint8_t system_i
* @brief Send a slugs_navigation message
* @param chan MAVLink channel to send the message
*
* @param u_m Measured Airspeed prior to the nav filter in m/s
* @param u_m Measured Airspeed prior to the nav filter
* @param phi_c Commanded Roll
* @param theta_c Commanded Pitch
* @param psiDot_c Commanded Turn rate
......@@ -213,7 +213,7 @@ static inline uint16_t mavlink_msg_slugs_navigation_encode_chan(uint8_t system_i
* @param dist2Go Remaining distance to Run on this leg of Navigation
* @param fromWP Origin WP
* @param toWP Destination WP
* @param h_c Commanded altitude in 0.1 m
* @param h_c Commanded altitude
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
......@@ -314,7 +314,7 @@ static inline void mavlink_msg_slugs_navigation_send_buf(mavlink_message_t *msgb
/**
* @brief Get field u_m from slugs_navigation message
*
* @return Measured Airspeed prior to the nav filter in m/s
* @return Measured Airspeed prior to the nav filter
*/
static inline float mavlink_msg_slugs_navigation_get_u_m(const mavlink_message_t* msg)
{
......@@ -404,7 +404,7 @@ static inline uint8_t mavlink_msg_slugs_navigation_get_toWP(const mavlink_messag
/**
* @brief Get field h_c from slugs_navigation message
*
* @return Commanded altitude in 0.1 m
* @return Commanded altitude
*/
static inline uint16_t mavlink_msg_slugs_navigation_get_h_c(const mavlink_message_t* msg)
{
......
......@@ -5,7 +5,7 @@
MAVPACKED(
typedef struct __mavlink_status_gps_t {
float magVar; /*< Magnetic variation, degrees */
float magVar; /*< Magnetic variation*/
uint16_t csFails; /*< Number of times checksum has failed*/
uint8_t gpsQuality; /*< The quality indicator, 0=fix not available or invalid, 1=GPS fix, 2=C/A differential GPS, 6=Dead reckoning mode, 7=Manual input mode (fixed position), 8=Simulator mode, 9= WAAS a*/
uint8_t msgsType; /*< Indicates if GN, GL or GP messages are being received*/
......@@ -63,7 +63,7 @@ typedef struct __mavlink_status_gps_t {
* @param gpsQuality The quality indicator, 0=fix not available or invalid, 1=GPS fix, 2=C/A differential GPS, 6=Dead reckoning mode, 7=Manual input mode (fixed position), 8=Simulator mode, 9= WAAS a
* @param msgsType Indicates if GN, GL or GP messages are being received
* @param posStatus A = data valid, V = data invalid
* @param magVar Magnetic variation, degrees
* @param magVar Magnetic variation
* @param magDir Magnetic variation direction E/W. Easterly variation (E) subtracts from True course and Westerly variation (W) adds to True course
* @param modeInd Positioning system mode indicator. A - Autonomous;D-Differential; E-Estimated (dead reckoning) mode;M-Manual input; N-Data not valid
* @return length of the message in bytes (excluding serial stream start sign)
......@@ -109,7 +109,7 @@ static inline uint16_t mavlink_msg_status_gps_pack(uint8_t system_id, uint8_t co
* @param gpsQuality The quality indicator, 0=fix not available or invalid, 1=GPS fix, 2=C/A differential GPS, 6=Dead reckoning mode, 7=Manual input mode (fixed position), 8=Simulator mode, 9= WAAS a
* @param msgsType Indicates if GN, GL or GP messages are being received
* @param posStatus A = data valid, V = data invalid
* @param magVar Magnetic variation, degrees
* @param magVar Magnetic variation
* @param magDir Magnetic variation direction E/W. Easterly variation (E) subtracts from True course and Westerly variation (W) adds to True course
* @param modeInd Positioning system mode indicator. A - Autonomous;D-Differential; E-Estimated (dead reckoning) mode;M-Manual input; N-Data not valid
* @return length of the message in bytes (excluding serial stream start sign)
......@@ -181,7 +181,7 @@ static inline uint16_t mavlink_msg_status_gps_encode_chan(uint8_t system_id, uin
* @param gpsQuality The quality indicator, 0=fix not available or invalid, 1=GPS fix, 2=C/A differential GPS, 6=Dead reckoning mode, 7=Manual input mode (fixed position), 8=Simulator mode, 9= WAAS a
* @param msgsType Indicates if GN, GL or GP messages are being received
* @param posStatus A = data valid, V = data invalid
* @param magVar Magnetic variation, degrees
* @param magVar Magnetic variation
* @param magDir Magnetic variation direction E/W. Easterly variation (E) subtracts from True course and Westerly variation (W) adds to True course
* @param modeInd Positioning system mode indicator. A - Autonomous;D-Differential; E-Estimated (dead reckoning) mode;M-Manual input; N-Data not valid
*/
......@@ -312,7 +312,7 @@ static inline uint8_t mavlink_msg_status_gps_get_posStatus(const mavlink_message
/**
* @brief Get field magVar from status_gps message
*
* @return Magnetic variation, degrees
* @return Magnetic variation
*/
static inline float mavlink_msg_status_gps_get_magVar(const mavlink_message_t* msg)
{
......
......@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed May 16 2018"
#define MAVLINK_BUILD_DATE "Fri May 18 2018"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
......
......@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed May 16 2018"
#define MAVLINK_BUILD_DATE "Fri May 18 2018"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
......
......@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed May 16 2018"
#define MAVLINK_BUILD_DATE "Fri May 18 2018"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 179
......
......@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed May 16 2018"
#define MAVLINK_BUILD_DATE "Fri May 18 2018"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
......
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