1dff1bfd33
【原 因】：更全更新 【过 程】： 【影 响】： # 类型 包含: # feat：新功能（feature） # fix：修补bug # docs：文档（documentation） # style： 格式（不影响代码运行的变动） # refactor：重构（即不是新增功能，也不是修改bug的代码变动） # test：增加测试 # chore：构建过程或辅助工具的变动
864 lines
39 KiB
C
864 lines
39 KiB
C
#pragma once
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// MESSAGE HIGH_LATENCY2 PACKING
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#define MAVLINK_MSG_ID_HIGH_LATENCY2 235
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MAVPACKED(
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typedef struct __mavlink_high_latency2_t {
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uint32_t timestamp; /*< [ms] Timestamp (milliseconds since boot or Unix epoch)*/
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int32_t latitude; /*< [degE7] Latitude*/
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int32_t longitude; /*< [degE7] Longitude*/
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uint16_t custom_mode; /*< A bitfield for use for autopilot-specific flags (2 byte version).*/
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int16_t altitude; /*< [m] Altitude above mean sea level*/
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int16_t target_altitude; /*< [m] Altitude setpoint*/
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uint16_t target_distance; /*< [dam] Distance to target waypoint or position*/
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uint16_t wp_num; /*< Current waypoint number*/
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uint16_t failure_flags; /*< Bitmap of failure flags.*/
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uint8_t type; /*< Type of the MAV (quadrotor, helicopter, etc.)*/
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uint8_t autopilot; /*< Autopilot type / class. Use MAV_AUTOPILOT_INVALID for components that are not flight controllers.*/
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uint8_t heading; /*< [deg/2] Heading*/
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uint8_t target_heading; /*< [deg/2] Heading setpoint*/
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uint8_t throttle; /*< [%] Throttle*/
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uint8_t airspeed; /*< [m/s*5] Airspeed*/
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uint8_t airspeed_sp; /*< [m/s*5] Airspeed setpoint*/
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uint8_t groundspeed; /*< [m/s*5] Groundspeed*/
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uint8_t windspeed; /*< [m/s*5] Windspeed*/
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uint8_t wind_heading; /*< [deg/2] Wind heading*/
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uint8_t eph; /*< [dm] Maximum error horizontal position since last message*/
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uint8_t epv; /*< [dm] Maximum error vertical position since last message*/
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int8_t temperature_air; /*< [degC] Air temperature from airspeed sensor*/
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int8_t climb_rate; /*< [dm/s] Maximum climb rate magnitude since last message*/
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int8_t battery; /*< [%] Battery level (-1 if field not provided).*/
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int8_t custom0; /*< Field for custom payload.*/
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int8_t custom1; /*< Field for custom payload.*/
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int8_t custom2; /*< Field for custom payload.*/
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}) mavlink_high_latency2_t;
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#define MAVLINK_MSG_ID_HIGH_LATENCY2_LEN 42
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#define MAVLINK_MSG_ID_HIGH_LATENCY2_MIN_LEN 42
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#define MAVLINK_MSG_ID_235_LEN 42
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#define MAVLINK_MSG_ID_235_MIN_LEN 42
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#define MAVLINK_MSG_ID_HIGH_LATENCY2_CRC 179
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#define MAVLINK_MSG_ID_235_CRC 179
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#if MAVLINK_COMMAND_24BIT
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#define MAVLINK_MESSAGE_INFO_HIGH_LATENCY2 { \
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235, \
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"HIGH_LATENCY2", \
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27, \
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{ { "timestamp", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_high_latency2_t, timestamp) }, \
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{ "type", NULL, MAVLINK_TYPE_UINT8_T, 0, 24, offsetof(mavlink_high_latency2_t, type) }, \
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{ "autopilot", NULL, MAVLINK_TYPE_UINT8_T, 0, 25, offsetof(mavlink_high_latency2_t, autopilot) }, \
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{ "custom_mode", NULL, MAVLINK_TYPE_UINT16_T, 0, 12, offsetof(mavlink_high_latency2_t, custom_mode) }, \
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{ "latitude", NULL, MAVLINK_TYPE_INT32_T, 0, 4, offsetof(mavlink_high_latency2_t, latitude) }, \
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{ "longitude", NULL, MAVLINK_TYPE_INT32_T, 0, 8, offsetof(mavlink_high_latency2_t, longitude) }, \
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{ "altitude", NULL, MAVLINK_TYPE_INT16_T, 0, 14, offsetof(mavlink_high_latency2_t, altitude) }, \
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{ "target_altitude", NULL, MAVLINK_TYPE_INT16_T, 0, 16, offsetof(mavlink_high_latency2_t, target_altitude) }, \
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{ "heading", NULL, MAVLINK_TYPE_UINT8_T, 0, 26, offsetof(mavlink_high_latency2_t, heading) }, \
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{ "target_heading", NULL, MAVLINK_TYPE_UINT8_T, 0, 27, offsetof(mavlink_high_latency2_t, target_heading) }, \
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{ "target_distance", NULL, MAVLINK_TYPE_UINT16_T, 0, 18, offsetof(mavlink_high_latency2_t, target_distance) }, \
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{ "throttle", NULL, MAVLINK_TYPE_UINT8_T, 0, 28, offsetof(mavlink_high_latency2_t, throttle) }, \
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{ "airspeed", NULL, MAVLINK_TYPE_UINT8_T, 0, 29, offsetof(mavlink_high_latency2_t, airspeed) }, \
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{ "airspeed_sp", NULL, MAVLINK_TYPE_UINT8_T, 0, 30, offsetof(mavlink_high_latency2_t, airspeed_sp) }, \
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{ "groundspeed", NULL, MAVLINK_TYPE_UINT8_T, 0, 31, offsetof(mavlink_high_latency2_t, groundspeed) }, \
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{ "windspeed", NULL, MAVLINK_TYPE_UINT8_T, 0, 32, offsetof(mavlink_high_latency2_t, windspeed) }, \
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{ "wind_heading", NULL, MAVLINK_TYPE_UINT8_T, 0, 33, offsetof(mavlink_high_latency2_t, wind_heading) }, \
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{ "eph", NULL, MAVLINK_TYPE_UINT8_T, 0, 34, offsetof(mavlink_high_latency2_t, eph) }, \
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{ "epv", NULL, MAVLINK_TYPE_UINT8_T, 0, 35, offsetof(mavlink_high_latency2_t, epv) }, \
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{ "temperature_air", NULL, MAVLINK_TYPE_INT8_T, 0, 36, offsetof(mavlink_high_latency2_t, temperature_air) }, \
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{ "climb_rate", NULL, MAVLINK_TYPE_INT8_T, 0, 37, offsetof(mavlink_high_latency2_t, climb_rate) }, \
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{ "battery", NULL, MAVLINK_TYPE_INT8_T, 0, 38, offsetof(mavlink_high_latency2_t, battery) }, \
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{ "wp_num", NULL, MAVLINK_TYPE_UINT16_T, 0, 20, offsetof(mavlink_high_latency2_t, wp_num) }, \
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{ "failure_flags", NULL, MAVLINK_TYPE_UINT16_T, 0, 22, offsetof(mavlink_high_latency2_t, failure_flags) }, \
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{ "custom0", NULL, MAVLINK_TYPE_INT8_T, 0, 39, offsetof(mavlink_high_latency2_t, custom0) }, \
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{ "custom1", NULL, MAVLINK_TYPE_INT8_T, 0, 40, offsetof(mavlink_high_latency2_t, custom1) }, \
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{ "custom2", NULL, MAVLINK_TYPE_INT8_T, 0, 41, offsetof(mavlink_high_latency2_t, custom2) }, \
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} \
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}
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#else
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#define MAVLINK_MESSAGE_INFO_HIGH_LATENCY2 { \
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"HIGH_LATENCY2", \
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27, \
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{ { "timestamp", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_high_latency2_t, timestamp) }, \
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{ "type", NULL, MAVLINK_TYPE_UINT8_T, 0, 24, offsetof(mavlink_high_latency2_t, type) }, \
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{ "autopilot", NULL, MAVLINK_TYPE_UINT8_T, 0, 25, offsetof(mavlink_high_latency2_t, autopilot) }, \
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{ "custom_mode", NULL, MAVLINK_TYPE_UINT16_T, 0, 12, offsetof(mavlink_high_latency2_t, custom_mode) }, \
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{ "latitude", NULL, MAVLINK_TYPE_INT32_T, 0, 4, offsetof(mavlink_high_latency2_t, latitude) }, \
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{ "longitude", NULL, MAVLINK_TYPE_INT32_T, 0, 8, offsetof(mavlink_high_latency2_t, longitude) }, \
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{ "altitude", NULL, MAVLINK_TYPE_INT16_T, 0, 14, offsetof(mavlink_high_latency2_t, altitude) }, \
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{ "target_altitude", NULL, MAVLINK_TYPE_INT16_T, 0, 16, offsetof(mavlink_high_latency2_t, target_altitude) }, \
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{ "heading", NULL, MAVLINK_TYPE_UINT8_T, 0, 26, offsetof(mavlink_high_latency2_t, heading) }, \
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{ "target_heading", NULL, MAVLINK_TYPE_UINT8_T, 0, 27, offsetof(mavlink_high_latency2_t, target_heading) }, \
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{ "target_distance", NULL, MAVLINK_TYPE_UINT16_T, 0, 18, offsetof(mavlink_high_latency2_t, target_distance) }, \
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{ "throttle", NULL, MAVLINK_TYPE_UINT8_T, 0, 28, offsetof(mavlink_high_latency2_t, throttle) }, \
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{ "airspeed", NULL, MAVLINK_TYPE_UINT8_T, 0, 29, offsetof(mavlink_high_latency2_t, airspeed) }, \
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{ "airspeed_sp", NULL, MAVLINK_TYPE_UINT8_T, 0, 30, offsetof(mavlink_high_latency2_t, airspeed_sp) }, \
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{ "groundspeed", NULL, MAVLINK_TYPE_UINT8_T, 0, 31, offsetof(mavlink_high_latency2_t, groundspeed) }, \
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{ "windspeed", NULL, MAVLINK_TYPE_UINT8_T, 0, 32, offsetof(mavlink_high_latency2_t, windspeed) }, \
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{ "wind_heading", NULL, MAVLINK_TYPE_UINT8_T, 0, 33, offsetof(mavlink_high_latency2_t, wind_heading) }, \
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{ "eph", NULL, MAVLINK_TYPE_UINT8_T, 0, 34, offsetof(mavlink_high_latency2_t, eph) }, \
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{ "epv", NULL, MAVLINK_TYPE_UINT8_T, 0, 35, offsetof(mavlink_high_latency2_t, epv) }, \
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{ "temperature_air", NULL, MAVLINK_TYPE_INT8_T, 0, 36, offsetof(mavlink_high_latency2_t, temperature_air) }, \
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{ "climb_rate", NULL, MAVLINK_TYPE_INT8_T, 0, 37, offsetof(mavlink_high_latency2_t, climb_rate) }, \
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{ "battery", NULL, MAVLINK_TYPE_INT8_T, 0, 38, offsetof(mavlink_high_latency2_t, battery) }, \
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{ "wp_num", NULL, MAVLINK_TYPE_UINT16_T, 0, 20, offsetof(mavlink_high_latency2_t, wp_num) }, \
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{ "failure_flags", NULL, MAVLINK_TYPE_UINT16_T, 0, 22, offsetof(mavlink_high_latency2_t, failure_flags) }, \
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{ "custom0", NULL, MAVLINK_TYPE_INT8_T, 0, 39, offsetof(mavlink_high_latency2_t, custom0) }, \
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{ "custom1", NULL, MAVLINK_TYPE_INT8_T, 0, 40, offsetof(mavlink_high_latency2_t, custom1) }, \
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{ "custom2", NULL, MAVLINK_TYPE_INT8_T, 0, 41, offsetof(mavlink_high_latency2_t, custom2) }, \
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} \
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}
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#endif
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/**
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* @brief Pack a high_latency2 message
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* @param system_id ID of this system
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* @param component_id ID of this component (e.g. 200 for IMU)
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* @param msg The MAVLink message to compress the data into
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*
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* @param timestamp [ms] Timestamp (milliseconds since boot or Unix epoch)
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* @param type Type of the MAV (quadrotor, helicopter, etc.)
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* @param autopilot Autopilot type / class. Use MAV_AUTOPILOT_INVALID for components that are not flight controllers.
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* @param custom_mode A bitfield for use for autopilot-specific flags (2 byte version).
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* @param latitude [degE7] Latitude
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* @param longitude [degE7] Longitude
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* @param altitude [m] Altitude above mean sea level
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* @param target_altitude [m] Altitude setpoint
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* @param heading [deg/2] Heading
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* @param target_heading [deg/2] Heading setpoint
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* @param target_distance [dam] Distance to target waypoint or position
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* @param throttle [%] Throttle
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* @param airspeed [m/s*5] Airspeed
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* @param airspeed_sp [m/s*5] Airspeed setpoint
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* @param groundspeed [m/s*5] Groundspeed
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* @param windspeed [m/s*5] Windspeed
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* @param wind_heading [deg/2] Wind heading
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* @param eph [dm] Maximum error horizontal position since last message
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* @param epv [dm] Maximum error vertical position since last message
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* @param temperature_air [degC] Air temperature from airspeed sensor
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* @param climb_rate [dm/s] Maximum climb rate magnitude since last message
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* @param battery [%] Battery level (-1 if field not provided).
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* @param wp_num Current waypoint number
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* @param failure_flags Bitmap of failure flags.
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* @param custom0 Field for custom payload.
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* @param custom1 Field for custom payload.
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* @param custom2 Field for custom payload.
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* @return length of the message in bytes (excluding serial stream start sign)
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*/
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static inline uint16_t mavlink_msg_high_latency2_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
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uint32_t timestamp, uint8_t type, uint8_t autopilot, uint16_t custom_mode, int32_t latitude, int32_t longitude, int16_t altitude, int16_t target_altitude, uint8_t heading, uint8_t target_heading, uint16_t target_distance, uint8_t throttle, uint8_t airspeed, uint8_t airspeed_sp, uint8_t groundspeed, uint8_t windspeed, uint8_t wind_heading, uint8_t eph, uint8_t epv, int8_t temperature_air, int8_t climb_rate, int8_t battery, uint16_t wp_num, uint16_t failure_flags, int8_t custom0, int8_t custom1, int8_t custom2)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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char buf[MAVLINK_MSG_ID_HIGH_LATENCY2_LEN];
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_mav_put_uint32_t(buf, 0, timestamp);
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_mav_put_int32_t(buf, 4, latitude);
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_mav_put_int32_t(buf, 8, longitude);
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_mav_put_uint16_t(buf, 12, custom_mode);
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_mav_put_int16_t(buf, 14, altitude);
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_mav_put_int16_t(buf, 16, target_altitude);
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_mav_put_uint16_t(buf, 18, target_distance);
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_mav_put_uint16_t(buf, 20, wp_num);
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_mav_put_uint16_t(buf, 22, failure_flags);
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_mav_put_uint8_t(buf, 24, type);
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_mav_put_uint8_t(buf, 25, autopilot);
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_mav_put_uint8_t(buf, 26, heading);
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_mav_put_uint8_t(buf, 27, target_heading);
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_mav_put_uint8_t(buf, 28, throttle);
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_mav_put_uint8_t(buf, 29, airspeed);
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_mav_put_uint8_t(buf, 30, airspeed_sp);
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_mav_put_uint8_t(buf, 31, groundspeed);
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_mav_put_uint8_t(buf, 32, windspeed);
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_mav_put_uint8_t(buf, 33, wind_heading);
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_mav_put_uint8_t(buf, 34, eph);
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_mav_put_uint8_t(buf, 35, epv);
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_mav_put_int8_t(buf, 36, temperature_air);
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_mav_put_int8_t(buf, 37, climb_rate);
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_mav_put_int8_t(buf, 38, battery);
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_mav_put_int8_t(buf, 39, custom0);
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_mav_put_int8_t(buf, 40, custom1);
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_mav_put_int8_t(buf, 41, custom2);
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_HIGH_LATENCY2_LEN);
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#else
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mavlink_high_latency2_t packet;
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packet.timestamp = timestamp;
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packet.latitude = latitude;
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packet.longitude = longitude;
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packet.custom_mode = custom_mode;
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packet.altitude = altitude;
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packet.target_altitude = target_altitude;
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packet.target_distance = target_distance;
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packet.wp_num = wp_num;
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packet.failure_flags = failure_flags;
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packet.type = type;
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packet.autopilot = autopilot;
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packet.heading = heading;
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packet.target_heading = target_heading;
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packet.throttle = throttle;
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packet.airspeed = airspeed;
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packet.airspeed_sp = airspeed_sp;
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packet.groundspeed = groundspeed;
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packet.windspeed = windspeed;
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packet.wind_heading = wind_heading;
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packet.eph = eph;
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packet.epv = epv;
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packet.temperature_air = temperature_air;
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packet.climb_rate = climb_rate;
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packet.battery = battery;
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packet.custom0 = custom0;
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packet.custom1 = custom1;
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packet.custom2 = custom2;
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_HIGH_LATENCY2_LEN);
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#endif
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msg->msgid = MAVLINK_MSG_ID_HIGH_LATENCY2;
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return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_HIGH_LATENCY2_MIN_LEN, MAVLINK_MSG_ID_HIGH_LATENCY2_LEN, MAVLINK_MSG_ID_HIGH_LATENCY2_CRC);
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}
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/**
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* @brief Pack a high_latency2 message on a channel
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* @param system_id ID of this system
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* @param component_id ID of this component (e.g. 200 for IMU)
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* @param chan The MAVLink channel this message will be sent over
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* @param msg The MAVLink message to compress the data into
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* @param timestamp [ms] Timestamp (milliseconds since boot or Unix epoch)
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* @param type Type of the MAV (quadrotor, helicopter, etc.)
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* @param autopilot Autopilot type / class. Use MAV_AUTOPILOT_INVALID for components that are not flight controllers.
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* @param custom_mode A bitfield for use for autopilot-specific flags (2 byte version).
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* @param latitude [degE7] Latitude
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* @param longitude [degE7] Longitude
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* @param altitude [m] Altitude above mean sea level
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* @param target_altitude [m] Altitude setpoint
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* @param heading [deg/2] Heading
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* @param target_heading [deg/2] Heading setpoint
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* @param target_distance [dam] Distance to target waypoint or position
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* @param throttle [%] Throttle
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* @param airspeed [m/s*5] Airspeed
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* @param airspeed_sp [m/s*5] Airspeed setpoint
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* @param groundspeed [m/s*5] Groundspeed
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* @param windspeed [m/s*5] Windspeed
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* @param wind_heading [deg/2] Wind heading
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* @param eph [dm] Maximum error horizontal position since last message
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* @param epv [dm] Maximum error vertical position since last message
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* @param temperature_air [degC] Air temperature from airspeed sensor
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* @param climb_rate [dm/s] Maximum climb rate magnitude since last message
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* @param battery [%] Battery level (-1 if field not provided).
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* @param wp_num Current waypoint number
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* @param failure_flags Bitmap of failure flags.
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* @param custom0 Field for custom payload.
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* @param custom1 Field for custom payload.
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* @param custom2 Field for custom payload.
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* @return length of the message in bytes (excluding serial stream start sign)
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*/
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static inline uint16_t mavlink_msg_high_latency2_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
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mavlink_message_t* msg,
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uint32_t timestamp,uint8_t type,uint8_t autopilot,uint16_t custom_mode,int32_t latitude,int32_t longitude,int16_t altitude,int16_t target_altitude,uint8_t heading,uint8_t target_heading,uint16_t target_distance,uint8_t throttle,uint8_t airspeed,uint8_t airspeed_sp,uint8_t groundspeed,uint8_t windspeed,uint8_t wind_heading,uint8_t eph,uint8_t epv,int8_t temperature_air,int8_t climb_rate,int8_t battery,uint16_t wp_num,uint16_t failure_flags,int8_t custom0,int8_t custom1,int8_t custom2)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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char buf[MAVLINK_MSG_ID_HIGH_LATENCY2_LEN];
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_mav_put_uint32_t(buf, 0, timestamp);
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_mav_put_int32_t(buf, 4, latitude);
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_mav_put_int32_t(buf, 8, longitude);
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_mav_put_uint16_t(buf, 12, custom_mode);
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_mav_put_int16_t(buf, 14, altitude);
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_mav_put_int16_t(buf, 16, target_altitude);
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_mav_put_uint16_t(buf, 18, target_distance);
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_mav_put_uint16_t(buf, 20, wp_num);
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_mav_put_uint16_t(buf, 22, failure_flags);
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_mav_put_uint8_t(buf, 24, type);
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_mav_put_uint8_t(buf, 25, autopilot);
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_mav_put_uint8_t(buf, 26, heading);
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_mav_put_uint8_t(buf, 27, target_heading);
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_mav_put_uint8_t(buf, 28, throttle);
|
|
_mav_put_uint8_t(buf, 29, airspeed);
|
|
_mav_put_uint8_t(buf, 30, airspeed_sp);
|
|
_mav_put_uint8_t(buf, 31, groundspeed);
|
|
_mav_put_uint8_t(buf, 32, windspeed);
|
|
_mav_put_uint8_t(buf, 33, wind_heading);
|
|
_mav_put_uint8_t(buf, 34, eph);
|
|
_mav_put_uint8_t(buf, 35, epv);
|
|
_mav_put_int8_t(buf, 36, temperature_air);
|
|
_mav_put_int8_t(buf, 37, climb_rate);
|
|
_mav_put_int8_t(buf, 38, battery);
|
|
_mav_put_int8_t(buf, 39, custom0);
|
|
_mav_put_int8_t(buf, 40, custom1);
|
|
_mav_put_int8_t(buf, 41, custom2);
|
|
|
|
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_HIGH_LATENCY2_LEN);
|
|
#else
|
|
mavlink_high_latency2_t packet;
|
|
packet.timestamp = timestamp;
|
|
packet.latitude = latitude;
|
|
packet.longitude = longitude;
|
|
packet.custom_mode = custom_mode;
|
|
packet.altitude = altitude;
|
|
packet.target_altitude = target_altitude;
|
|
packet.target_distance = target_distance;
|
|
packet.wp_num = wp_num;
|
|
packet.failure_flags = failure_flags;
|
|
packet.type = type;
|
|
packet.autopilot = autopilot;
|
|
packet.heading = heading;
|
|
packet.target_heading = target_heading;
|
|
packet.throttle = throttle;
|
|
packet.airspeed = airspeed;
|
|
packet.airspeed_sp = airspeed_sp;
|
|
packet.groundspeed = groundspeed;
|
|
packet.windspeed = windspeed;
|
|
packet.wind_heading = wind_heading;
|
|
packet.eph = eph;
|
|
packet.epv = epv;
|
|
packet.temperature_air = temperature_air;
|
|
packet.climb_rate = climb_rate;
|
|
packet.battery = battery;
|
|
packet.custom0 = custom0;
|
|
packet.custom1 = custom1;
|
|
packet.custom2 = custom2;
|
|
|
|
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_HIGH_LATENCY2_LEN);
|
|
#endif
|
|
|
|
msg->msgid = MAVLINK_MSG_ID_HIGH_LATENCY2;
|
|
return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_HIGH_LATENCY2_MIN_LEN, MAVLINK_MSG_ID_HIGH_LATENCY2_LEN, MAVLINK_MSG_ID_HIGH_LATENCY2_CRC);
|
|
}
|
|
|
|
/**
|
|
* @brief Encode a high_latency2 struct
|
|
*
|
|
* @param system_id ID of this system
|
|
* @param component_id ID of this component (e.g. 200 for IMU)
|
|
* @param msg The MAVLink message to compress the data into
|
|
* @param high_latency2 C-struct to read the message contents from
|
|
*/
|
|
static inline uint16_t mavlink_msg_high_latency2_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_high_latency2_t* high_latency2)
|
|
{
|
|
return mavlink_msg_high_latency2_pack(system_id, component_id, msg, high_latency2->timestamp, high_latency2->type, high_latency2->autopilot, high_latency2->custom_mode, high_latency2->latitude, high_latency2->longitude, high_latency2->altitude, high_latency2->target_altitude, high_latency2->heading, high_latency2->target_heading, high_latency2->target_distance, high_latency2->throttle, high_latency2->airspeed, high_latency2->airspeed_sp, high_latency2->groundspeed, high_latency2->windspeed, high_latency2->wind_heading, high_latency2->eph, high_latency2->epv, high_latency2->temperature_air, high_latency2->climb_rate, high_latency2->battery, high_latency2->wp_num, high_latency2->failure_flags, high_latency2->custom0, high_latency2->custom1, high_latency2->custom2);
|
|
}
|
|
|
|
/**
|
|
* @brief Encode a high_latency2 struct on a channel
|
|
*
|
|
* @param system_id ID of this system
|
|
* @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 high_latency2 C-struct to read the message contents from
|
|
*/
|
|
static inline uint16_t mavlink_msg_high_latency2_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_high_latency2_t* high_latency2)
|
|
{
|
|
return mavlink_msg_high_latency2_pack_chan(system_id, component_id, chan, msg, high_latency2->timestamp, high_latency2->type, high_latency2->autopilot, high_latency2->custom_mode, high_latency2->latitude, high_latency2->longitude, high_latency2->altitude, high_latency2->target_altitude, high_latency2->heading, high_latency2->target_heading, high_latency2->target_distance, high_latency2->throttle, high_latency2->airspeed, high_latency2->airspeed_sp, high_latency2->groundspeed, high_latency2->windspeed, high_latency2->wind_heading, high_latency2->eph, high_latency2->epv, high_latency2->temperature_air, high_latency2->climb_rate, high_latency2->battery, high_latency2->wp_num, high_latency2->failure_flags, high_latency2->custom0, high_latency2->custom1, high_latency2->custom2);
|
|
}
|
|
|
|
/**
|
|
* @brief Send a high_latency2 message
|
|
* @param chan MAVLink channel to send the message
|
|
*
|
|
* @param timestamp [ms] Timestamp (milliseconds since boot or Unix epoch)
|
|
* @param type Type of the MAV (quadrotor, helicopter, etc.)
|
|
* @param autopilot Autopilot type / class. Use MAV_AUTOPILOT_INVALID for components that are not flight controllers.
|
|
* @param custom_mode A bitfield for use for autopilot-specific flags (2 byte version).
|
|
* @param latitude [degE7] Latitude
|
|
* @param longitude [degE7] Longitude
|
|
* @param altitude [m] Altitude above mean sea level
|
|
* @param target_altitude [m] Altitude setpoint
|
|
* @param heading [deg/2] Heading
|
|
* @param target_heading [deg/2] Heading setpoint
|
|
* @param target_distance [dam] Distance to target waypoint or position
|
|
* @param throttle [%] Throttle
|
|
* @param airspeed [m/s*5] Airspeed
|
|
* @param airspeed_sp [m/s*5] Airspeed setpoint
|
|
* @param groundspeed [m/s*5] Groundspeed
|
|
* @param windspeed [m/s*5] Windspeed
|
|
* @param wind_heading [deg/2] Wind heading
|
|
* @param eph [dm] Maximum error horizontal position since last message
|
|
* @param epv [dm] Maximum error vertical position since last message
|
|
* @param temperature_air [degC] Air temperature from airspeed sensor
|
|
* @param climb_rate [dm/s] Maximum climb rate magnitude since last message
|
|
* @param battery [%] Battery level (-1 if field not provided).
|
|
* @param wp_num Current waypoint number
|
|
* @param failure_flags Bitmap of failure flags.
|
|
* @param custom0 Field for custom payload.
|
|
* @param custom1 Field for custom payload.
|
|
* @param custom2 Field for custom payload.
|
|
*/
|
|
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
|
|
|
|
static inline void mavlink_msg_high_latency2_send(mavlink_channel_t chan, uint32_t timestamp, uint8_t type, uint8_t autopilot, uint16_t custom_mode, int32_t latitude, int32_t longitude, int16_t altitude, int16_t target_altitude, uint8_t heading, uint8_t target_heading, uint16_t target_distance, uint8_t throttle, uint8_t airspeed, uint8_t airspeed_sp, uint8_t groundspeed, uint8_t windspeed, uint8_t wind_heading, uint8_t eph, uint8_t epv, int8_t temperature_air, int8_t climb_rate, int8_t battery, uint16_t wp_num, uint16_t failure_flags, int8_t custom0, int8_t custom1, int8_t custom2)
|
|
{
|
|
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
|
|
char buf[MAVLINK_MSG_ID_HIGH_LATENCY2_LEN];
|
|
_mav_put_uint32_t(buf, 0, timestamp);
|
|
_mav_put_int32_t(buf, 4, latitude);
|
|
_mav_put_int32_t(buf, 8, longitude);
|
|
_mav_put_uint16_t(buf, 12, custom_mode);
|
|
_mav_put_int16_t(buf, 14, altitude);
|
|
_mav_put_int16_t(buf, 16, target_altitude);
|
|
_mav_put_uint16_t(buf, 18, target_distance);
|
|
_mav_put_uint16_t(buf, 20, wp_num);
|
|
_mav_put_uint16_t(buf, 22, failure_flags);
|
|
_mav_put_uint8_t(buf, 24, type);
|
|
_mav_put_uint8_t(buf, 25, autopilot);
|
|
_mav_put_uint8_t(buf, 26, heading);
|
|
_mav_put_uint8_t(buf, 27, target_heading);
|
|
_mav_put_uint8_t(buf, 28, throttle);
|
|
_mav_put_uint8_t(buf, 29, airspeed);
|
|
_mav_put_uint8_t(buf, 30, airspeed_sp);
|
|
_mav_put_uint8_t(buf, 31, groundspeed);
|
|
_mav_put_uint8_t(buf, 32, windspeed);
|
|
_mav_put_uint8_t(buf, 33, wind_heading);
|
|
_mav_put_uint8_t(buf, 34, eph);
|
|
_mav_put_uint8_t(buf, 35, epv);
|
|
_mav_put_int8_t(buf, 36, temperature_air);
|
|
_mav_put_int8_t(buf, 37, climb_rate);
|
|
_mav_put_int8_t(buf, 38, battery);
|
|
_mav_put_int8_t(buf, 39, custom0);
|
|
_mav_put_int8_t(buf, 40, custom1);
|
|
_mav_put_int8_t(buf, 41, custom2);
|
|
|
|
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIGH_LATENCY2, buf, MAVLINK_MSG_ID_HIGH_LATENCY2_MIN_LEN, MAVLINK_MSG_ID_HIGH_LATENCY2_LEN, MAVLINK_MSG_ID_HIGH_LATENCY2_CRC);
|
|
#else
|
|
mavlink_high_latency2_t packet;
|
|
packet.timestamp = timestamp;
|
|
packet.latitude = latitude;
|
|
packet.longitude = longitude;
|
|
packet.custom_mode = custom_mode;
|
|
packet.altitude = altitude;
|
|
packet.target_altitude = target_altitude;
|
|
packet.target_distance = target_distance;
|
|
packet.wp_num = wp_num;
|
|
packet.failure_flags = failure_flags;
|
|
packet.type = type;
|
|
packet.autopilot = autopilot;
|
|
packet.heading = heading;
|
|
packet.target_heading = target_heading;
|
|
packet.throttle = throttle;
|
|
packet.airspeed = airspeed;
|
|
packet.airspeed_sp = airspeed_sp;
|
|
packet.groundspeed = groundspeed;
|
|
packet.windspeed = windspeed;
|
|
packet.wind_heading = wind_heading;
|
|
packet.eph = eph;
|
|
packet.epv = epv;
|
|
packet.temperature_air = temperature_air;
|
|
packet.climb_rate = climb_rate;
|
|
packet.battery = battery;
|
|
packet.custom0 = custom0;
|
|
packet.custom1 = custom1;
|
|
packet.custom2 = custom2;
|
|
|
|
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIGH_LATENCY2, (const char *)&packet, MAVLINK_MSG_ID_HIGH_LATENCY2_MIN_LEN, MAVLINK_MSG_ID_HIGH_LATENCY2_LEN, MAVLINK_MSG_ID_HIGH_LATENCY2_CRC);
|
|
#endif
|
|
}
|
|
|
|
/**
|
|
* @brief Send a high_latency2 message
|
|
* @param chan MAVLink channel to send the message
|
|
* @param struct The MAVLink struct to serialize
|
|
*/
|
|
static inline void mavlink_msg_high_latency2_send_struct(mavlink_channel_t chan, const mavlink_high_latency2_t* high_latency2)
|
|
{
|
|
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
|
|
mavlink_msg_high_latency2_send(chan, high_latency2->timestamp, high_latency2->type, high_latency2->autopilot, high_latency2->custom_mode, high_latency2->latitude, high_latency2->longitude, high_latency2->altitude, high_latency2->target_altitude, high_latency2->heading, high_latency2->target_heading, high_latency2->target_distance, high_latency2->throttle, high_latency2->airspeed, high_latency2->airspeed_sp, high_latency2->groundspeed, high_latency2->windspeed, high_latency2->wind_heading, high_latency2->eph, high_latency2->epv, high_latency2->temperature_air, high_latency2->climb_rate, high_latency2->battery, high_latency2->wp_num, high_latency2->failure_flags, high_latency2->custom0, high_latency2->custom1, high_latency2->custom2);
|
|
#else
|
|
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIGH_LATENCY2, (const char *)high_latency2, MAVLINK_MSG_ID_HIGH_LATENCY2_MIN_LEN, MAVLINK_MSG_ID_HIGH_LATENCY2_LEN, MAVLINK_MSG_ID_HIGH_LATENCY2_CRC);
|
|
#endif
|
|
}
|
|
|
|
#if MAVLINK_MSG_ID_HIGH_LATENCY2_LEN <= MAVLINK_MAX_PAYLOAD_LEN
|
|
/*
|
|
This varient of _send() can be used to save stack space by re-using
|
|
memory from the receive buffer. The caller provides a
|
|
mavlink_message_t which is the size of a full mavlink message. This
|
|
is usually the receive buffer for the channel, and allows a reply to an
|
|
incoming message with minimum stack space usage.
|
|
*/
|
|
static inline void mavlink_msg_high_latency2_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t timestamp, uint8_t type, uint8_t autopilot, uint16_t custom_mode, int32_t latitude, int32_t longitude, int16_t altitude, int16_t target_altitude, uint8_t heading, uint8_t target_heading, uint16_t target_distance, uint8_t throttle, uint8_t airspeed, uint8_t airspeed_sp, uint8_t groundspeed, uint8_t windspeed, uint8_t wind_heading, uint8_t eph, uint8_t epv, int8_t temperature_air, int8_t climb_rate, int8_t battery, uint16_t wp_num, uint16_t failure_flags, int8_t custom0, int8_t custom1, int8_t custom2)
|
|
{
|
|
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
|
|
char *buf = (char *)msgbuf;
|
|
_mav_put_uint32_t(buf, 0, timestamp);
|
|
_mav_put_int32_t(buf, 4, latitude);
|
|
_mav_put_int32_t(buf, 8, longitude);
|
|
_mav_put_uint16_t(buf, 12, custom_mode);
|
|
_mav_put_int16_t(buf, 14, altitude);
|
|
_mav_put_int16_t(buf, 16, target_altitude);
|
|
_mav_put_uint16_t(buf, 18, target_distance);
|
|
_mav_put_uint16_t(buf, 20, wp_num);
|
|
_mav_put_uint16_t(buf, 22, failure_flags);
|
|
_mav_put_uint8_t(buf, 24, type);
|
|
_mav_put_uint8_t(buf, 25, autopilot);
|
|
_mav_put_uint8_t(buf, 26, heading);
|
|
_mav_put_uint8_t(buf, 27, target_heading);
|
|
_mav_put_uint8_t(buf, 28, throttle);
|
|
_mav_put_uint8_t(buf, 29, airspeed);
|
|
_mav_put_uint8_t(buf, 30, airspeed_sp);
|
|
_mav_put_uint8_t(buf, 31, groundspeed);
|
|
_mav_put_uint8_t(buf, 32, windspeed);
|
|
_mav_put_uint8_t(buf, 33, wind_heading);
|
|
_mav_put_uint8_t(buf, 34, eph);
|
|
_mav_put_uint8_t(buf, 35, epv);
|
|
_mav_put_int8_t(buf, 36, temperature_air);
|
|
_mav_put_int8_t(buf, 37, climb_rate);
|
|
_mav_put_int8_t(buf, 38, battery);
|
|
_mav_put_int8_t(buf, 39, custom0);
|
|
_mav_put_int8_t(buf, 40, custom1);
|
|
_mav_put_int8_t(buf, 41, custom2);
|
|
|
|
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIGH_LATENCY2, buf, MAVLINK_MSG_ID_HIGH_LATENCY2_MIN_LEN, MAVLINK_MSG_ID_HIGH_LATENCY2_LEN, MAVLINK_MSG_ID_HIGH_LATENCY2_CRC);
|
|
#else
|
|
mavlink_high_latency2_t *packet = (mavlink_high_latency2_t *)msgbuf;
|
|
packet->timestamp = timestamp;
|
|
packet->latitude = latitude;
|
|
packet->longitude = longitude;
|
|
packet->custom_mode = custom_mode;
|
|
packet->altitude = altitude;
|
|
packet->target_altitude = target_altitude;
|
|
packet->target_distance = target_distance;
|
|
packet->wp_num = wp_num;
|
|
packet->failure_flags = failure_flags;
|
|
packet->type = type;
|
|
packet->autopilot = autopilot;
|
|
packet->heading = heading;
|
|
packet->target_heading = target_heading;
|
|
packet->throttle = throttle;
|
|
packet->airspeed = airspeed;
|
|
packet->airspeed_sp = airspeed_sp;
|
|
packet->groundspeed = groundspeed;
|
|
packet->windspeed = windspeed;
|
|
packet->wind_heading = wind_heading;
|
|
packet->eph = eph;
|
|
packet->epv = epv;
|
|
packet->temperature_air = temperature_air;
|
|
packet->climb_rate = climb_rate;
|
|
packet->battery = battery;
|
|
packet->custom0 = custom0;
|
|
packet->custom1 = custom1;
|
|
packet->custom2 = custom2;
|
|
|
|
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIGH_LATENCY2, (const char *)packet, MAVLINK_MSG_ID_HIGH_LATENCY2_MIN_LEN, MAVLINK_MSG_ID_HIGH_LATENCY2_LEN, MAVLINK_MSG_ID_HIGH_LATENCY2_CRC);
|
|
#endif
|
|
}
|
|
#endif
|
|
|
|
#endif
|
|
|
|
// MESSAGE HIGH_LATENCY2 UNPACKING
|
|
|
|
|
|
/**
|
|
* @brief Get field timestamp from high_latency2 message
|
|
*
|
|
* @return [ms] Timestamp (milliseconds since boot or Unix epoch)
|
|
*/
|
|
static inline uint32_t mavlink_msg_high_latency2_get_timestamp(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint32_t(msg, 0);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field type from high_latency2 message
|
|
*
|
|
* @return Type of the MAV (quadrotor, helicopter, etc.)
|
|
*/
|
|
static inline uint8_t mavlink_msg_high_latency2_get_type(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint8_t(msg, 24);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field autopilot from high_latency2 message
|
|
*
|
|
* @return Autopilot type / class. Use MAV_AUTOPILOT_INVALID for components that are not flight controllers.
|
|
*/
|
|
static inline uint8_t mavlink_msg_high_latency2_get_autopilot(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint8_t(msg, 25);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field custom_mode from high_latency2 message
|
|
*
|
|
* @return A bitfield for use for autopilot-specific flags (2 byte version).
|
|
*/
|
|
static inline uint16_t mavlink_msg_high_latency2_get_custom_mode(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint16_t(msg, 12);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field latitude from high_latency2 message
|
|
*
|
|
* @return [degE7] Latitude
|
|
*/
|
|
static inline int32_t mavlink_msg_high_latency2_get_latitude(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int32_t(msg, 4);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field longitude from high_latency2 message
|
|
*
|
|
* @return [degE7] Longitude
|
|
*/
|
|
static inline int32_t mavlink_msg_high_latency2_get_longitude(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int32_t(msg, 8);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field altitude from high_latency2 message
|
|
*
|
|
* @return [m] Altitude above mean sea level
|
|
*/
|
|
static inline int16_t mavlink_msg_high_latency2_get_altitude(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int16_t(msg, 14);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field target_altitude from high_latency2 message
|
|
*
|
|
* @return [m] Altitude setpoint
|
|
*/
|
|
static inline int16_t mavlink_msg_high_latency2_get_target_altitude(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int16_t(msg, 16);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field heading from high_latency2 message
|
|
*
|
|
* @return [deg/2] Heading
|
|
*/
|
|
static inline uint8_t mavlink_msg_high_latency2_get_heading(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint8_t(msg, 26);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field target_heading from high_latency2 message
|
|
*
|
|
* @return [deg/2] Heading setpoint
|
|
*/
|
|
static inline uint8_t mavlink_msg_high_latency2_get_target_heading(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint8_t(msg, 27);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field target_distance from high_latency2 message
|
|
*
|
|
* @return [dam] Distance to target waypoint or position
|
|
*/
|
|
static inline uint16_t mavlink_msg_high_latency2_get_target_distance(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint16_t(msg, 18);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field throttle from high_latency2 message
|
|
*
|
|
* @return [%] Throttle
|
|
*/
|
|
static inline uint8_t mavlink_msg_high_latency2_get_throttle(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint8_t(msg, 28);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field airspeed from high_latency2 message
|
|
*
|
|
* @return [m/s*5] Airspeed
|
|
*/
|
|
static inline uint8_t mavlink_msg_high_latency2_get_airspeed(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint8_t(msg, 29);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field airspeed_sp from high_latency2 message
|
|
*
|
|
* @return [m/s*5] Airspeed setpoint
|
|
*/
|
|
static inline uint8_t mavlink_msg_high_latency2_get_airspeed_sp(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint8_t(msg, 30);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field groundspeed from high_latency2 message
|
|
*
|
|
* @return [m/s*5] Groundspeed
|
|
*/
|
|
static inline uint8_t mavlink_msg_high_latency2_get_groundspeed(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint8_t(msg, 31);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field windspeed from high_latency2 message
|
|
*
|
|
* @return [m/s*5] Windspeed
|
|
*/
|
|
static inline uint8_t mavlink_msg_high_latency2_get_windspeed(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint8_t(msg, 32);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field wind_heading from high_latency2 message
|
|
*
|
|
* @return [deg/2] Wind heading
|
|
*/
|
|
static inline uint8_t mavlink_msg_high_latency2_get_wind_heading(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint8_t(msg, 33);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field eph from high_latency2 message
|
|
*
|
|
* @return [dm] Maximum error horizontal position since last message
|
|
*/
|
|
static inline uint8_t mavlink_msg_high_latency2_get_eph(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint8_t(msg, 34);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field epv from high_latency2 message
|
|
*
|
|
* @return [dm] Maximum error vertical position since last message
|
|
*/
|
|
static inline uint8_t mavlink_msg_high_latency2_get_epv(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint8_t(msg, 35);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field temperature_air from high_latency2 message
|
|
*
|
|
* @return [degC] Air temperature from airspeed sensor
|
|
*/
|
|
static inline int8_t mavlink_msg_high_latency2_get_temperature_air(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int8_t(msg, 36);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field climb_rate from high_latency2 message
|
|
*
|
|
* @return [dm/s] Maximum climb rate magnitude since last message
|
|
*/
|
|
static inline int8_t mavlink_msg_high_latency2_get_climb_rate(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int8_t(msg, 37);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field battery from high_latency2 message
|
|
*
|
|
* @return [%] Battery level (-1 if field not provided).
|
|
*/
|
|
static inline int8_t mavlink_msg_high_latency2_get_battery(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int8_t(msg, 38);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field wp_num from high_latency2 message
|
|
*
|
|
* @return Current waypoint number
|
|
*/
|
|
static inline uint16_t mavlink_msg_high_latency2_get_wp_num(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint16_t(msg, 20);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field failure_flags from high_latency2 message
|
|
*
|
|
* @return Bitmap of failure flags.
|
|
*/
|
|
static inline uint16_t mavlink_msg_high_latency2_get_failure_flags(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_uint16_t(msg, 22);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field custom0 from high_latency2 message
|
|
*
|
|
* @return Field for custom payload.
|
|
*/
|
|
static inline int8_t mavlink_msg_high_latency2_get_custom0(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int8_t(msg, 39);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field custom1 from high_latency2 message
|
|
*
|
|
* @return Field for custom payload.
|
|
*/
|
|
static inline int8_t mavlink_msg_high_latency2_get_custom1(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int8_t(msg, 40);
|
|
}
|
|
|
|
/**
|
|
* @brief Get field custom2 from high_latency2 message
|
|
*
|
|
* @return Field for custom payload.
|
|
*/
|
|
static inline int8_t mavlink_msg_high_latency2_get_custom2(const mavlink_message_t* msg)
|
|
{
|
|
return _MAV_RETURN_int8_t(msg, 41);
|
|
}
|
|
|
|
/**
|
|
* @brief Decode a high_latency2 message into a struct
|
|
*
|
|
* @param msg The message to decode
|
|
* @param high_latency2 C-struct to decode the message contents into
|
|
*/
|
|
static inline void mavlink_msg_high_latency2_decode(const mavlink_message_t* msg, mavlink_high_latency2_t* high_latency2)
|
|
{
|
|
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
|
|
high_latency2->timestamp = mavlink_msg_high_latency2_get_timestamp(msg);
|
|
high_latency2->latitude = mavlink_msg_high_latency2_get_latitude(msg);
|
|
high_latency2->longitude = mavlink_msg_high_latency2_get_longitude(msg);
|
|
high_latency2->custom_mode = mavlink_msg_high_latency2_get_custom_mode(msg);
|
|
high_latency2->altitude = mavlink_msg_high_latency2_get_altitude(msg);
|
|
high_latency2->target_altitude = mavlink_msg_high_latency2_get_target_altitude(msg);
|
|
high_latency2->target_distance = mavlink_msg_high_latency2_get_target_distance(msg);
|
|
high_latency2->wp_num = mavlink_msg_high_latency2_get_wp_num(msg);
|
|
high_latency2->failure_flags = mavlink_msg_high_latency2_get_failure_flags(msg);
|
|
high_latency2->type = mavlink_msg_high_latency2_get_type(msg);
|
|
high_latency2->autopilot = mavlink_msg_high_latency2_get_autopilot(msg);
|
|
high_latency2->heading = mavlink_msg_high_latency2_get_heading(msg);
|
|
high_latency2->target_heading = mavlink_msg_high_latency2_get_target_heading(msg);
|
|
high_latency2->throttle = mavlink_msg_high_latency2_get_throttle(msg);
|
|
high_latency2->airspeed = mavlink_msg_high_latency2_get_airspeed(msg);
|
|
high_latency2->airspeed_sp = mavlink_msg_high_latency2_get_airspeed_sp(msg);
|
|
high_latency2->groundspeed = mavlink_msg_high_latency2_get_groundspeed(msg);
|
|
high_latency2->windspeed = mavlink_msg_high_latency2_get_windspeed(msg);
|
|
high_latency2->wind_heading = mavlink_msg_high_latency2_get_wind_heading(msg);
|
|
high_latency2->eph = mavlink_msg_high_latency2_get_eph(msg);
|
|
high_latency2->epv = mavlink_msg_high_latency2_get_epv(msg);
|
|
high_latency2->temperature_air = mavlink_msg_high_latency2_get_temperature_air(msg);
|
|
high_latency2->climb_rate = mavlink_msg_high_latency2_get_climb_rate(msg);
|
|
high_latency2->battery = mavlink_msg_high_latency2_get_battery(msg);
|
|
high_latency2->custom0 = mavlink_msg_high_latency2_get_custom0(msg);
|
|
high_latency2->custom1 = mavlink_msg_high_latency2_get_custom1(msg);
|
|
high_latency2->custom2 = mavlink_msg_high_latency2_get_custom2(msg);
|
|
#else
|
|
uint8_t len = msg->len < MAVLINK_MSG_ID_HIGH_LATENCY2_LEN? msg->len : MAVLINK_MSG_ID_HIGH_LATENCY2_LEN;
|
|
memset(high_latency2, 0, MAVLINK_MSG_ID_HIGH_LATENCY2_LEN);
|
|
memcpy(high_latency2, _MAV_PAYLOAD(msg), len);
|
|
#endif
|
|
}
|