diff options
Diffstat (limited to 'mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_controls.h')
-rw-r--r-- | mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_controls.h | 364 |
1 files changed, 364 insertions, 0 deletions
diff --git a/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_controls.h b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_controls.h new file mode 100644 index 000000000..41a9bc949 --- /dev/null +++ b/mavlink/include/mavlink/v1.0/common/mavlink_msg_hil_controls.h @@ -0,0 +1,364 @@ +// 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 +} |