cr929 first release
This commit is contained in:
matt
@@ -0,0 +1,463 @@
|
||||
#pragma once
|
||||
// MESSAGE HIL_CONTROLS PACKING
|
||||
|
||||
#define MAVLINK_MSG_ID_HIL_CONTROLS 91
|
||||
|
||||
|
||||
typedef struct __mavlink_hil_controls_t {
|
||||
uint32_t time_usec; /*< [us] Timestamp (UNIX Epoch time or time since system boot). The receiving end can infer timestamp format (since 1.1.1970 or since system boot) by checking for the magnitude of the number.*/
|
||||
float roll_ailerons; /*< Control output -1 .. 1*/
|
||||
float pitch_elevator; /*< Control output -1 .. 1*/
|
||||
float yaw_rudder; /*< Control output -1 .. 1*/
|
||||
float throttle; /*< Throttle 0 .. 1*/
|
||||
float aux1; /*< Aux 1, -1 .. 1*/
|
||||
float aux2; /*< Aux 2, -1 .. 1*/
|
||||
float aux3; /*< Aux 3, -1 .. 1*/
|
||||
float aux4; /*< Aux 4, -1 .. 1*/
|
||||
uint8_t mode; /*< System mode.*/
|
||||
uint8_t nav_mode; /*< Navigation mode (MAV_NAV_MODE)*/
|
||||
} mavlink_hil_controls_t;
|
||||
|
||||
#define MAVLINK_MSG_ID_HIL_CONTROLS_LEN 38
|
||||
#define MAVLINK_MSG_ID_HIL_CONTROLS_MIN_LEN 38
|
||||
#define MAVLINK_MSG_ID_91_LEN 38
|
||||
#define MAVLINK_MSG_ID_91_MIN_LEN 38
|
||||
|
||||
#define MAVLINK_MSG_ID_HIL_CONTROLS_CRC 187
|
||||
#define MAVLINK_MSG_ID_91_CRC 187
|
||||
|
||||
|
||||
|
||||
#if MAVLINK_COMMAND_24BIT
|
||||
#define MAVLINK_MESSAGE_INFO_HIL_CONTROLS { \
|
||||
91, \
|
||||
"HIL_CONTROLS", \
|
||||
11, \
|
||||
{ { "time_usec", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_hil_controls_t, time_usec) }, \
|
||||
{ "roll_ailerons", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_hil_controls_t, roll_ailerons) }, \
|
||||
{ "pitch_elevator", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_hil_controls_t, pitch_elevator) }, \
|
||||
{ "yaw_rudder", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_hil_controls_t, yaw_rudder) }, \
|
||||
{ "throttle", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_hil_controls_t, throttle) }, \
|
||||
{ "aux1", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_hil_controls_t, aux1) }, \
|
||||
{ "aux2", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_hil_controls_t, aux2) }, \
|
||||
{ "aux3", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_hil_controls_t, aux3) }, \
|
||||
{ "aux4", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_hil_controls_t, aux4) }, \
|
||||
{ "mode", NULL, MAVLINK_TYPE_UINT8_T, 0, 36, offsetof(mavlink_hil_controls_t, mode) }, \
|
||||
{ "nav_mode", NULL, MAVLINK_TYPE_UINT8_T, 0, 37, offsetof(mavlink_hil_controls_t, nav_mode) }, \
|
||||
} \
|
||||
}
|
||||
#else
|
||||
#define MAVLINK_MESSAGE_INFO_HIL_CONTROLS { \
|
||||
"HIL_CONTROLS", \
|
||||
11, \
|
||||
{ { "time_usec", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_hil_controls_t, time_usec) }, \
|
||||
{ "roll_ailerons", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_hil_controls_t, roll_ailerons) }, \
|
||||
{ "pitch_elevator", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_hil_controls_t, pitch_elevator) }, \
|
||||
{ "yaw_rudder", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_hil_controls_t, yaw_rudder) }, \
|
||||
{ "throttle", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_hil_controls_t, throttle) }, \
|
||||
{ "aux1", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_hil_controls_t, aux1) }, \
|
||||
{ "aux2", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_hil_controls_t, aux2) }, \
|
||||
{ "aux3", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_hil_controls_t, aux3) }, \
|
||||
{ "aux4", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_hil_controls_t, aux4) }, \
|
||||
{ "mode", NULL, MAVLINK_TYPE_UINT8_T, 0, 36, offsetof(mavlink_hil_controls_t, mode) }, \
|
||||
{ "nav_mode", NULL, MAVLINK_TYPE_UINT8_T, 0, 37, offsetof(mavlink_hil_controls_t, nav_mode) }, \
|
||||
} \
|
||||
}
|
||||
#endif
|
||||
|
||||
/**
|
||||
* @brief Pack a hil_controls message
|
||||
* @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 time_usec [us] Timestamp (UNIX Epoch time or time since system boot). The receiving end can infer timestamp format (since 1.1.1970 or since system boot) by checking for the magnitude of the number.
|
||||
* @param roll_ailerons Control output -1 .. 1
|
||||
* @param pitch_elevator Control output -1 .. 1
|
||||
* @param yaw_rudder Control output -1 .. 1
|
||||
* @param throttle Throttle 0 .. 1
|
||||
* @param aux1 Aux 1, -1 .. 1
|
||||
* @param aux2 Aux 2, -1 .. 1
|
||||
* @param aux3 Aux 3, -1 .. 1
|
||||
* @param aux4 Aux 4, -1 .. 1
|
||||
* @param mode System mode.
|
||||
* @param nav_mode Navigation mode (MAV_NAV_MODE)
|
||||
* @return length of the message in bytes (excluding serial stream start sign)
|
||||
*/
|
||||
static inline uint16_t mavlink_msg_hil_controls_pack(uint16_t system_id, uint8_t component_id, mavlink_message_t* msg,
|
||||
uint32_t time_usec, float roll_ailerons, float pitch_elevator, float yaw_rudder, float throttle, float aux1, float aux2, float aux3, float aux4, uint8_t mode, uint8_t nav_mode)
|
||||
{
|
||||
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
|
||||
char buf[MAVLINK_MSG_ID_HIL_CONTROLS_LEN];
|
||||
_mav_put_uint32_t(buf, 0, time_usec);
|
||||
_mav_put_float(buf, 4, roll_ailerons);
|
||||
_mav_put_float(buf, 8, pitch_elevator);
|
||||
_mav_put_float(buf, 12, yaw_rudder);
|
||||
_mav_put_float(buf, 16, throttle);
|
||||
_mav_put_float(buf, 20, aux1);
|
||||
_mav_put_float(buf, 24, aux2);
|
||||
_mav_put_float(buf, 28, aux3);
|
||||
_mav_put_float(buf, 32, aux4);
|
||||
_mav_put_uint8_t(buf, 36, mode);
|
||||
_mav_put_uint8_t(buf, 37, nav_mode);
|
||||
|
||||
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_HIL_CONTROLS_LEN);
|
||||
#else
|
||||
mavlink_hil_controls_t packet;
|
||||
packet.time_usec = time_usec;
|
||||
packet.roll_ailerons = roll_ailerons;
|
||||
packet.pitch_elevator = pitch_elevator;
|
||||
packet.yaw_rudder = yaw_rudder;
|
||||
packet.throttle = throttle;
|
||||
packet.aux1 = aux1;
|
||||
packet.aux2 = aux2;
|
||||
packet.aux3 = aux3;
|
||||
packet.aux4 = aux4;
|
||||
packet.mode = mode;
|
||||
packet.nav_mode = nav_mode;
|
||||
|
||||
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_HIL_CONTROLS_LEN);
|
||||
#endif
|
||||
|
||||
msg->msgid = MAVLINK_MSG_ID_HIL_CONTROLS;
|
||||
return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_HIL_CONTROLS_MIN_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_CRC);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Pack a hil_controls message 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 time_usec [us] Timestamp (UNIX Epoch time or time since system boot). The receiving end can infer timestamp format (since 1.1.1970 or since system boot) by checking for the magnitude of the number.
|
||||
* @param roll_ailerons Control output -1 .. 1
|
||||
* @param pitch_elevator Control output -1 .. 1
|
||||
* @param yaw_rudder Control output -1 .. 1
|
||||
* @param throttle Throttle 0 .. 1
|
||||
* @param aux1 Aux 1, -1 .. 1
|
||||
* @param aux2 Aux 2, -1 .. 1
|
||||
* @param aux3 Aux 3, -1 .. 1
|
||||
* @param aux4 Aux 4, -1 .. 1
|
||||
* @param mode System mode.
|
||||
* @param nav_mode Navigation mode (MAV_NAV_MODE)
|
||||
* @return length of the message in bytes (excluding serial stream start sign)
|
||||
*/
|
||||
static inline uint16_t mavlink_msg_hil_controls_pack_chan(uint16_t system_id, uint8_t component_id, uint8_t chan,
|
||||
mavlink_message_t* msg,
|
||||
uint32_t time_usec,float roll_ailerons,float pitch_elevator,float yaw_rudder,float throttle,float aux1,float aux2,float aux3,float aux4,uint8_t mode,uint8_t nav_mode)
|
||||
{
|
||||
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
|
||||
char buf[MAVLINK_MSG_ID_HIL_CONTROLS_LEN];
|
||||
_mav_put_uint32_t(buf, 0, time_usec);
|
||||
_mav_put_float(buf, 4, roll_ailerons);
|
||||
_mav_put_float(buf, 8, pitch_elevator);
|
||||
_mav_put_float(buf, 12, yaw_rudder);
|
||||
_mav_put_float(buf, 16, throttle);
|
||||
_mav_put_float(buf, 20, aux1);
|
||||
_mav_put_float(buf, 24, aux2);
|
||||
_mav_put_float(buf, 28, aux3);
|
||||
_mav_put_float(buf, 32, aux4);
|
||||
_mav_put_uint8_t(buf, 36, mode);
|
||||
_mav_put_uint8_t(buf, 37, nav_mode);
|
||||
|
||||
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_HIL_CONTROLS_LEN);
|
||||
#else
|
||||
mavlink_hil_controls_t packet;
|
||||
packet.time_usec = time_usec;
|
||||
packet.roll_ailerons = roll_ailerons;
|
||||
packet.pitch_elevator = pitch_elevator;
|
||||
packet.yaw_rudder = yaw_rudder;
|
||||
packet.throttle = throttle;
|
||||
packet.aux1 = aux1;
|
||||
packet.aux2 = aux2;
|
||||
packet.aux3 = aux3;
|
||||
packet.aux4 = aux4;
|
||||
packet.mode = mode;
|
||||
packet.nav_mode = nav_mode;
|
||||
|
||||
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_HIL_CONTROLS_LEN);
|
||||
#endif
|
||||
|
||||
msg->msgid = MAVLINK_MSG_ID_HIL_CONTROLS;
|
||||
return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_HIL_CONTROLS_MIN_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_CRC);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Encode a hil_controls 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 hil_controls C-struct to read the message contents from
|
||||
*/
|
||||
static inline uint16_t mavlink_msg_hil_controls_encode(uint16_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_hil_controls_t* hil_controls)
|
||||
{
|
||||
return mavlink_msg_hil_controls_pack(system_id, component_id, msg, hil_controls->time_usec, hil_controls->roll_ailerons, hil_controls->pitch_elevator, hil_controls->yaw_rudder, hil_controls->throttle, hil_controls->aux1, hil_controls->aux2, hil_controls->aux3, hil_controls->aux4, hil_controls->mode, hil_controls->nav_mode);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Encode a hil_controls 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 hil_controls C-struct to read the message contents from
|
||||
*/
|
||||
static inline uint16_t mavlink_msg_hil_controls_encode_chan(uint16_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_hil_controls_t* hil_controls)
|
||||
{
|
||||
return mavlink_msg_hil_controls_pack_chan(system_id, component_id, chan, msg, hil_controls->time_usec, hil_controls->roll_ailerons, hil_controls->pitch_elevator, hil_controls->yaw_rudder, hil_controls->throttle, hil_controls->aux1, hil_controls->aux2, hil_controls->aux3, hil_controls->aux4, hil_controls->mode, hil_controls->nav_mode);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Send a hil_controls message
|
||||
* @param chan MAVLink channel to send the message
|
||||
*
|
||||
* @param time_usec [us] Timestamp (UNIX Epoch time or time since system boot). The receiving end can infer timestamp format (since 1.1.1970 or since system boot) by checking for the magnitude of the number.
|
||||
* @param roll_ailerons Control output -1 .. 1
|
||||
* @param pitch_elevator Control output -1 .. 1
|
||||
* @param yaw_rudder Control output -1 .. 1
|
||||
* @param throttle Throttle 0 .. 1
|
||||
* @param aux1 Aux 1, -1 .. 1
|
||||
* @param aux2 Aux 2, -1 .. 1
|
||||
* @param aux3 Aux 3, -1 .. 1
|
||||
* @param aux4 Aux 4, -1 .. 1
|
||||
* @param mode System mode.
|
||||
* @param nav_mode Navigation mode (MAV_NAV_MODE)
|
||||
*/
|
||||
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
|
||||
|
||||
static inline void mavlink_msg_hil_controls_send(mavlink_channel_t chan, uint32_t time_usec, float roll_ailerons, float pitch_elevator, float yaw_rudder, float throttle, float aux1, float aux2, float aux3, float aux4, uint8_t mode, uint8_t nav_mode)
|
||||
{
|
||||
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
|
||||
char buf[MAVLINK_MSG_ID_HIL_CONTROLS_LEN];
|
||||
_mav_put_uint32_t(buf, 0, time_usec);
|
||||
_mav_put_float(buf, 4, roll_ailerons);
|
||||
_mav_put_float(buf, 8, pitch_elevator);
|
||||
_mav_put_float(buf, 12, yaw_rudder);
|
||||
_mav_put_float(buf, 16, throttle);
|
||||
_mav_put_float(buf, 20, aux1);
|
||||
_mav_put_float(buf, 24, aux2);
|
||||
_mav_put_float(buf, 28, aux3);
|
||||
_mav_put_float(buf, 32, aux4);
|
||||
_mav_put_uint8_t(buf, 36, mode);
|
||||
_mav_put_uint8_t(buf, 37, nav_mode);
|
||||
|
||||
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_CONTROLS, buf, MAVLINK_MSG_ID_HIL_CONTROLS_MIN_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_CRC);
|
||||
#else
|
||||
mavlink_hil_controls_t packet;
|
||||
packet.time_usec = time_usec;
|
||||
packet.roll_ailerons = roll_ailerons;
|
||||
packet.pitch_elevator = pitch_elevator;
|
||||
packet.yaw_rudder = yaw_rudder;
|
||||
packet.throttle = throttle;
|
||||
packet.aux1 = aux1;
|
||||
packet.aux2 = aux2;
|
||||
packet.aux3 = aux3;
|
||||
packet.aux4 = aux4;
|
||||
packet.mode = mode;
|
||||
packet.nav_mode = nav_mode;
|
||||
|
||||
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_CONTROLS, (const char *)&packet, MAVLINK_MSG_ID_HIL_CONTROLS_MIN_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_CRC);
|
||||
#endif
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Send a hil_controls message
|
||||
* @param chan MAVLink channel to send the message
|
||||
* @param struct The MAVLink struct to serialize
|
||||
*/
|
||||
static inline void mavlink_msg_hil_controls_send_struct(mavlink_channel_t chan, const mavlink_hil_controls_t* hil_controls)
|
||||
{
|
||||
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
|
||||
mavlink_msg_hil_controls_send(chan, hil_controls->time_usec, hil_controls->roll_ailerons, hil_controls->pitch_elevator, hil_controls->yaw_rudder, hil_controls->throttle, hil_controls->aux1, hil_controls->aux2, hil_controls->aux3, hil_controls->aux4, hil_controls->mode, hil_controls->nav_mode);
|
||||
#else
|
||||
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_CONTROLS, (const char *)hil_controls, MAVLINK_MSG_ID_HIL_CONTROLS_MIN_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_CRC);
|
||||
#endif
|
||||
}
|
||||
|
||||
#if MAVLINK_MSG_ID_HIL_CONTROLS_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_hil_controls_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t time_usec, float roll_ailerons, float pitch_elevator, float yaw_rudder, float throttle, float aux1, float aux2, float aux3, float aux4, uint8_t mode, uint8_t nav_mode)
|
||||
{
|
||||
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
|
||||
char *buf = (char *)msgbuf;
|
||||
_mav_put_uint32_t(buf, 0, time_usec);
|
||||
_mav_put_float(buf, 4, roll_ailerons);
|
||||
_mav_put_float(buf, 8, pitch_elevator);
|
||||
_mav_put_float(buf, 12, yaw_rudder);
|
||||
_mav_put_float(buf, 16, throttle);
|
||||
_mav_put_float(buf, 20, aux1);
|
||||
_mav_put_float(buf, 24, aux2);
|
||||
_mav_put_float(buf, 28, aux3);
|
||||
_mav_put_float(buf, 32, aux4);
|
||||
_mav_put_uint8_t(buf, 36, mode);
|
||||
_mav_put_uint8_t(buf, 37, nav_mode);
|
||||
|
||||
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_CONTROLS, buf, MAVLINK_MSG_ID_HIL_CONTROLS_MIN_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_CRC);
|
||||
#else
|
||||
mavlink_hil_controls_t *packet = (mavlink_hil_controls_t *)msgbuf;
|
||||
packet->time_usec = time_usec;
|
||||
packet->roll_ailerons = roll_ailerons;
|
||||
packet->pitch_elevator = pitch_elevator;
|
||||
packet->yaw_rudder = yaw_rudder;
|
||||
packet->throttle = throttle;
|
||||
packet->aux1 = aux1;
|
||||
packet->aux2 = aux2;
|
||||
packet->aux3 = aux3;
|
||||
packet->aux4 = aux4;
|
||||
packet->mode = mode;
|
||||
packet->nav_mode = nav_mode;
|
||||
|
||||
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_CONTROLS, (const char *)packet, MAVLINK_MSG_ID_HIL_CONTROLS_MIN_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_LEN, MAVLINK_MSG_ID_HIL_CONTROLS_CRC);
|
||||
#endif
|
||||
}
|
||||
#endif
|
||||
|
||||
#endif
|
||||
|
||||
// MESSAGE HIL_CONTROLS UNPACKING
|
||||
|
||||
|
||||
/**
|
||||
* @brief Get field time_usec from hil_controls message
|
||||
*
|
||||
* @return [us] Timestamp (UNIX Epoch time or time since system boot). The receiving end can infer timestamp format (since 1.1.1970 or since system boot) by checking for the magnitude of the number.
|
||||
*/
|
||||
static inline uint32_t mavlink_msg_hil_controls_get_time_usec(const mavlink_message_t* msg)
|
||||
{
|
||||
return _MAV_RETURN_uint32_t(msg, 0);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Get field roll_ailerons from hil_controls message
|
||||
*
|
||||
* @return Control output -1 .. 1
|
||||
*/
|
||||
static inline float mavlink_msg_hil_controls_get_roll_ailerons(const mavlink_message_t* msg)
|
||||
{
|
||||
return _MAV_RETURN_float(msg, 4);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Get field pitch_elevator from hil_controls message
|
||||
*
|
||||
* @return Control output -1 .. 1
|
||||
*/
|
||||
static inline float mavlink_msg_hil_controls_get_pitch_elevator(const mavlink_message_t* msg)
|
||||
{
|
||||
return _MAV_RETURN_float(msg, 8);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Get field yaw_rudder from hil_controls message
|
||||
*
|
||||
* @return Control output -1 .. 1
|
||||
*/
|
||||
static inline float mavlink_msg_hil_controls_get_yaw_rudder(const mavlink_message_t* msg)
|
||||
{
|
||||
return _MAV_RETURN_float(msg, 12);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Get field throttle from hil_controls message
|
||||
*
|
||||
* @return Throttle 0 .. 1
|
||||
*/
|
||||
static inline float mavlink_msg_hil_controls_get_throttle(const mavlink_message_t* msg)
|
||||
{
|
||||
return _MAV_RETURN_float(msg, 16);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Get field aux1 from hil_controls message
|
||||
*
|
||||
* @return Aux 1, -1 .. 1
|
||||
*/
|
||||
static inline float mavlink_msg_hil_controls_get_aux1(const mavlink_message_t* msg)
|
||||
{
|
||||
return _MAV_RETURN_float(msg, 20);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Get field aux2 from hil_controls message
|
||||
*
|
||||
* @return Aux 2, -1 .. 1
|
||||
*/
|
||||
static inline float mavlink_msg_hil_controls_get_aux2(const mavlink_message_t* msg)
|
||||
{
|
||||
return _MAV_RETURN_float(msg, 24);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Get field aux3 from hil_controls message
|
||||
*
|
||||
* @return Aux 3, -1 .. 1
|
||||
*/
|
||||
static inline float mavlink_msg_hil_controls_get_aux3(const mavlink_message_t* msg)
|
||||
{
|
||||
return _MAV_RETURN_float(msg, 28);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Get field aux4 from hil_controls message
|
||||
*
|
||||
* @return Aux 4, -1 .. 1
|
||||
*/
|
||||
static inline float mavlink_msg_hil_controls_get_aux4(const mavlink_message_t* msg)
|
||||
{
|
||||
return _MAV_RETURN_float(msg, 32);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Get field mode from hil_controls message
|
||||
*
|
||||
* @return System mode.
|
||||
*/
|
||||
static inline uint8_t mavlink_msg_hil_controls_get_mode(const mavlink_message_t* msg)
|
||||
{
|
||||
return _MAV_RETURN_uint8_t(msg, 36);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Get field nav_mode from hil_controls message
|
||||
*
|
||||
* @return Navigation mode (MAV_NAV_MODE)
|
||||
*/
|
||||
static inline uint8_t mavlink_msg_hil_controls_get_nav_mode(const mavlink_message_t* msg)
|
||||
{
|
||||
return _MAV_RETURN_uint8_t(msg, 37);
|
||||
}
|
||||
|
||||
/**
|
||||
* @brief Decode a hil_controls message into a struct
|
||||
*
|
||||
* @param msg The message to decode
|
||||
* @param hil_controls C-struct to decode the message contents into
|
||||
*/
|
||||
static inline void mavlink_msg_hil_controls_decode(const mavlink_message_t* msg, mavlink_hil_controls_t* hil_controls)
|
||||
{
|
||||
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
|
||||
hil_controls->time_usec = mavlink_msg_hil_controls_get_time_usec(msg);
|
||||
hil_controls->roll_ailerons = mavlink_msg_hil_controls_get_roll_ailerons(msg);
|
||||
hil_controls->pitch_elevator = mavlink_msg_hil_controls_get_pitch_elevator(msg);
|
||||
hil_controls->yaw_rudder = mavlink_msg_hil_controls_get_yaw_rudder(msg);
|
||||
hil_controls->throttle = mavlink_msg_hil_controls_get_throttle(msg);
|
||||
hil_controls->aux1 = mavlink_msg_hil_controls_get_aux1(msg);
|
||||
hil_controls->aux2 = mavlink_msg_hil_controls_get_aux2(msg);
|
||||
hil_controls->aux3 = mavlink_msg_hil_controls_get_aux3(msg);
|
||||
hil_controls->aux4 = mavlink_msg_hil_controls_get_aux4(msg);
|
||||
hil_controls->mode = mavlink_msg_hil_controls_get_mode(msg);
|
||||
hil_controls->nav_mode = mavlink_msg_hil_controls_get_nav_mode(msg);
|
||||
#else
|
||||
uint8_t len = msg->len < MAVLINK_MSG_ID_HIL_CONTROLS_LEN? msg->len : MAVLINK_MSG_ID_HIL_CONTROLS_LEN;
|
||||
memset(hil_controls, 0, MAVLINK_MSG_ID_HIL_CONTROLS_LEN);
|
||||
memcpy(hil_controls, _MAV_PAYLOAD(msg), len);
|
||||
#endif
|
||||
}
|
||||
Reference in New Issue
Block a user