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// MESSAGE HIL_CONTROLS PACKING
#define MAVLINK_MSG_ID_HIL_CONTROLS 91
typedef struct __mavlink_hil_controls_t
{
uint64_t time_usec; ///< Timestamp (microseconds since UNIX epoch or microseconds since system boot)
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 (MAV_MODE)
uint8_t nav_mode; ///< Navigation mode (MAV_NAV_MODE)
} mavlink_hil_controls_t;
#define MAVLINK_MSG_ID_HIL_CONTROLS_LEN 42
#define MAVLINK_MSG_ID_91_LEN 42
#define MAVLINK_MESSAGE_INFO_HIL_CONTROLS { \
"HIL_CONTROLS", \
11, \
{ { "time_usec", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_hil_controls_t, time_usec) }, \
{ "roll_ailerons", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_hil_controls_t, roll_ailerons) }, \
{ "pitch_elevator", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_hil_controls_t, pitch_elevator) }, \
{ "yaw_rudder", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_hil_controls_t, yaw_rudder) }, \
{ "throttle", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_hil_controls_t, throttle) }, \
{ "aux1", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_hil_controls_t, aux1) }, \
{ "aux2", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_hil_controls_t, aux2) }, \
{ "aux3", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_hil_controls_t, aux3) }, \
{ "aux4", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_hil_controls_t, aux4) }, \
{ "mode", NULL, MAVLINK_TYPE_UINT8_T, 0, 40, offsetof(mavlink_hil_controls_t, mode) }, \
{ "nav_mode", NULL, MAVLINK_TYPE_UINT8_T, 0, 41, offsetof(mavlink_hil_controls_t, nav_mode) }, \
} \
}
/**
* @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 Timestamp (microseconds since UNIX epoch or microseconds since system boot)
* @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 (MAV_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(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
uint64_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[42];
_mav_put_uint64_t(buf, 0, time_usec);
_mav_put_float(buf, 8, roll_ailerons);
_mav_put_float(buf, 12, pitch_elevator);
_mav_put_float(buf, 16, yaw_rudder);
_mav_put_float(buf, 20, throttle);
_mav_put_float(buf, 24, aux1);
_mav_put_float(buf, 28, aux2);
_mav_put_float(buf, 32, aux3);
_mav_put_float(buf, 36, aux4);
_mav_put_uint8_t(buf, 40, mode);
_mav_put_uint8_t(buf, 41, nav_mode);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, 42);
#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, 42);
#endif
msg->msgid = MAVLINK_MSG_ID_HIL_CONTROLS;
return mavlink_finalize_message(msg, system_id, component_id, 42, 63);
}
/**
* @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 was sent over
* @param msg The MAVLink message to compress the data into
* @param time_usec Timestamp (microseconds since UNIX epoch or microseconds since system boot)
* @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 (MAV_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(uint8_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
uint64_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[42];
_mav_put_uint64_t(buf, 0, time_usec);
_mav_put_float(buf, 8, roll_ailerons);
_mav_put_float(buf, 12, pitch_elevator);
_mav_put_float(buf, 16, yaw_rudder);
_mav_put_float(buf, 20, throttle);
_mav_put_float(buf, 24, aux1);
_mav_put_float(buf, 28, aux2);
_mav_put_float(buf, 32, aux3);
_mav_put_float(buf, 36, aux4);
_mav_put_uint8_t(buf, 40, mode);
_mav_put_uint8_t(buf, 41, nav_mode);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, 42);
#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, 42);
#endif
msg->msgid = MAVLINK_MSG_ID_HIL_CONTROLS;
return mavlink_finalize_message_chan(msg, system_id, component_id, chan, 42, 63);
}
/**
* @brief Encode a hil_controls struct into a 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 hil_controls C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_hil_controls_encode(uint8_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 Send a hil_controls message
* @param chan MAVLink channel to send the message
*
* @param time_usec Timestamp (microseconds since UNIX epoch or microseconds since system boot)
* @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 (MAV_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, uint64_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[42];
_mav_put_uint64_t(buf, 0, time_usec);
_mav_put_float(buf, 8, roll_ailerons);
_mav_put_float(buf, 12, pitch_elevator);
_mav_put_float(buf, 16, yaw_rudder);
_mav_put_float(buf, 20, throttle);
_mav_put_float(buf, 24, aux1);
_mav_put_float(buf, 28, aux2);
_mav_put_float(buf, 32, aux3);
_mav_put_float(buf, 36, aux4);
_mav_put_uint8_t(buf, 40, mode);
_mav_put_uint8_t(buf, 41, nav_mode);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_CONTROLS, buf, 42, 63);
#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, 42, 63);
#endif
}
#endif
// MESSAGE HIL_CONTROLS UNPACKING
/**
* @brief Get field time_usec from hil_controls message
*
* @return Timestamp (microseconds since UNIX epoch or microseconds since system boot)
*/
static inline uint64_t mavlink_msg_hil_controls_get_time_usec(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint64_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, 8);
}
/**
* @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, 12);
}
/**
* @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, 16);
}
/**
* @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, 20);
}
/**
* @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, 24);
}
/**
* @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, 28);
}
/**
* @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, 32);
}
/**
* @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, 36);
}
/**
* @brief Get field mode from hil_controls message
*
* @return System mode (MAV_MODE)
*/
static inline uint8_t mavlink_msg_hil_controls_get_mode(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 40);
}
/**
* @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, 41);
}
/**
* @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
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
memcpy(hil_controls, _MAV_PAYLOAD(msg), 42);
#endif
}