#pragma once // MESSAGE RADIO_CALIBRATION PACKING #define MAVLINK_MSG_ID_RADIO_CALIBRATION 221 typedef struct __mavlink_radio_calibration_t { uint16_t aileron[3]; /*< Aileron setpoints: left, center, right*/ uint16_t elevator[3]; /*< Elevator setpoints: nose down, center, nose up*/ uint16_t rudder[3]; /*< Rudder setpoints: nose left, center, nose right*/ uint16_t gyro[2]; /*< Tail gyro mode/gain setpoints: heading hold, rate mode*/ uint16_t pitch[5]; /*< Pitch curve setpoints (every 25%)*/ uint16_t throttle[5]; /*< Throttle curve setpoints (every 25%)*/ } mavlink_radio_calibration_t; #define MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN 42 #define MAVLINK_MSG_ID_RADIO_CALIBRATION_MIN_LEN 42 #define MAVLINK_MSG_ID_221_LEN 42 #define MAVLINK_MSG_ID_221_MIN_LEN 42 #define MAVLINK_MSG_ID_RADIO_CALIBRATION_CRC 71 #define MAVLINK_MSG_ID_221_CRC 71 #define MAVLINK_MSG_RADIO_CALIBRATION_FIELD_AILERON_LEN 3 #define MAVLINK_MSG_RADIO_CALIBRATION_FIELD_ELEVATOR_LEN 3 #define MAVLINK_MSG_RADIO_CALIBRATION_FIELD_RUDDER_LEN 3 #define MAVLINK_MSG_RADIO_CALIBRATION_FIELD_GYRO_LEN 2 #define MAVLINK_MSG_RADIO_CALIBRATION_FIELD_PITCH_LEN 5 #define MAVLINK_MSG_RADIO_CALIBRATION_FIELD_THROTTLE_LEN 5 #if MAVLINK_COMMAND_24BIT #define MAVLINK_MESSAGE_INFO_RADIO_CALIBRATION { \ 221, \ "RADIO_CALIBRATION", \ 6, \ { { "aileron", NULL, MAVLINK_TYPE_UINT16_T, 3, 0, offsetof(mavlink_radio_calibration_t, aileron) }, \ { "elevator", NULL, MAVLINK_TYPE_UINT16_T, 3, 6, offsetof(mavlink_radio_calibration_t, elevator) }, \ { "rudder", NULL, MAVLINK_TYPE_UINT16_T, 3, 12, offsetof(mavlink_radio_calibration_t, rudder) }, \ { "gyro", NULL, MAVLINK_TYPE_UINT16_T, 2, 18, offsetof(mavlink_radio_calibration_t, gyro) }, \ { "pitch", NULL, MAVLINK_TYPE_UINT16_T, 5, 22, offsetof(mavlink_radio_calibration_t, pitch) }, \ { "throttle", NULL, MAVLINK_TYPE_UINT16_T, 5, 32, offsetof(mavlink_radio_calibration_t, throttle) }, \ } \ } #else #define MAVLINK_MESSAGE_INFO_RADIO_CALIBRATION { \ "RADIO_CALIBRATION", \ 6, \ { { "aileron", NULL, MAVLINK_TYPE_UINT16_T, 3, 0, offsetof(mavlink_radio_calibration_t, aileron) }, \ { "elevator", NULL, MAVLINK_TYPE_UINT16_T, 3, 6, offsetof(mavlink_radio_calibration_t, elevator) }, \ { "rudder", NULL, MAVLINK_TYPE_UINT16_T, 3, 12, offsetof(mavlink_radio_calibration_t, rudder) }, \ { "gyro", NULL, MAVLINK_TYPE_UINT16_T, 2, 18, offsetof(mavlink_radio_calibration_t, gyro) }, \ { "pitch", NULL, MAVLINK_TYPE_UINT16_T, 5, 22, offsetof(mavlink_radio_calibration_t, pitch) }, \ { "throttle", NULL, MAVLINK_TYPE_UINT16_T, 5, 32, offsetof(mavlink_radio_calibration_t, throttle) }, \ } \ } #endif /** * @brief Pack a radio_calibration 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 aileron Aileron setpoints: left, center, right * @param elevator Elevator setpoints: nose down, center, nose up * @param rudder Rudder setpoints: nose left, center, nose right * @param gyro Tail gyro mode/gain setpoints: heading hold, rate mode * @param pitch Pitch curve setpoints (every 25%) * @param throttle Throttle curve setpoints (every 25%) * @return length of the message in bytes (excluding serial stream start sign) */ static inline uint16_t mavlink_msg_radio_calibration_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const uint16_t *aileron, const uint16_t *elevator, const uint16_t *rudder, const uint16_t *gyro, const uint16_t *pitch, const uint16_t *throttle) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN]; _mav_put_uint16_t_array(buf, 0, aileron, 3); _mav_put_uint16_t_array(buf, 6, elevator, 3); _mav_put_uint16_t_array(buf, 12, rudder, 3); _mav_put_uint16_t_array(buf, 18, gyro, 2); _mav_put_uint16_t_array(buf, 22, pitch, 5); _mav_put_uint16_t_array(buf, 32, throttle, 5); memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN); #else mavlink_radio_calibration_t packet; mav_array_memcpy(packet.aileron, aileron, sizeof(uint16_t)*3); mav_array_memcpy(packet.elevator, elevator, sizeof(uint16_t)*3); mav_array_memcpy(packet.rudder, rudder, sizeof(uint16_t)*3); mav_array_memcpy(packet.gyro, gyro, sizeof(uint16_t)*2); mav_array_memcpy(packet.pitch, pitch, sizeof(uint16_t)*5); mav_array_memcpy(packet.throttle, throttle, sizeof(uint16_t)*5); memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN); #endif msg->msgid = MAVLINK_MSG_ID_RADIO_CALIBRATION; return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_RADIO_CALIBRATION_MIN_LEN, MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN, MAVLINK_MSG_ID_RADIO_CALIBRATION_CRC); } /** * @brief Pack a radio_calibration 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 aileron Aileron setpoints: left, center, right * @param elevator Elevator setpoints: nose down, center, nose up * @param rudder Rudder setpoints: nose left, center, nose right * @param gyro Tail gyro mode/gain setpoints: heading hold, rate mode * @param pitch Pitch curve setpoints (every 25%) * @param throttle Throttle curve setpoints (every 25%) * @return length of the message in bytes (excluding serial stream start sign) */ static inline uint16_t mavlink_msg_radio_calibration_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const uint16_t *aileron,const uint16_t *elevator,const uint16_t *rudder,const uint16_t *gyro,const uint16_t *pitch,const uint16_t *throttle) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN]; _mav_put_uint16_t_array(buf, 0, aileron, 3); _mav_put_uint16_t_array(buf, 6, elevator, 3); _mav_put_uint16_t_array(buf, 12, rudder, 3); _mav_put_uint16_t_array(buf, 18, gyro, 2); _mav_put_uint16_t_array(buf, 22, pitch, 5); _mav_put_uint16_t_array(buf, 32, throttle, 5); memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN); #else mavlink_radio_calibration_t packet; mav_array_memcpy(packet.aileron, aileron, sizeof(uint16_t)*3); mav_array_memcpy(packet.elevator, elevator, sizeof(uint16_t)*3); mav_array_memcpy(packet.rudder, rudder, sizeof(uint16_t)*3); mav_array_memcpy(packet.gyro, gyro, sizeof(uint16_t)*2); mav_array_memcpy(packet.pitch, pitch, sizeof(uint16_t)*5); mav_array_memcpy(packet.throttle, throttle, sizeof(uint16_t)*5); memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN); #endif msg->msgid = MAVLINK_MSG_ID_RADIO_CALIBRATION; return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_RADIO_CALIBRATION_MIN_LEN, MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN, MAVLINK_MSG_ID_RADIO_CALIBRATION_CRC); } /** * @brief Encode a radio_calibration 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 radio_calibration C-struct to read the message contents from */ static inline uint16_t mavlink_msg_radio_calibration_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_radio_calibration_t* radio_calibration) { return mavlink_msg_radio_calibration_pack(system_id, component_id, msg, radio_calibration->aileron, radio_calibration->elevator, radio_calibration->rudder, radio_calibration->gyro, radio_calibration->pitch, radio_calibration->throttle); } /** * @brief Encode a radio_calibration 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 radio_calibration C-struct to read the message contents from */ static inline uint16_t mavlink_msg_radio_calibration_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_radio_calibration_t* radio_calibration) { return mavlink_msg_radio_calibration_pack_chan(system_id, component_id, chan, msg, radio_calibration->aileron, radio_calibration->elevator, radio_calibration->rudder, radio_calibration->gyro, radio_calibration->pitch, radio_calibration->throttle); } /** * @brief Send a radio_calibration message * @param chan MAVLink channel to send the message * * @param aileron Aileron setpoints: left, center, right * @param elevator Elevator setpoints: nose down, center, nose up * @param rudder Rudder setpoints: nose left, center, nose right * @param gyro Tail gyro mode/gain setpoints: heading hold, rate mode * @param pitch Pitch curve setpoints (every 25%) * @param throttle Throttle curve setpoints (every 25%) */ #ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS static inline void mavlink_msg_radio_calibration_send(mavlink_channel_t chan, const uint16_t *aileron, const uint16_t *elevator, const uint16_t *rudder, const uint16_t *gyro, const uint16_t *pitch, const uint16_t *throttle) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN]; _mav_put_uint16_t_array(buf, 0, aileron, 3); _mav_put_uint16_t_array(buf, 6, elevator, 3); _mav_put_uint16_t_array(buf, 12, rudder, 3); _mav_put_uint16_t_array(buf, 18, gyro, 2); _mav_put_uint16_t_array(buf, 22, pitch, 5); _mav_put_uint16_t_array(buf, 32, throttle, 5); _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RADIO_CALIBRATION, buf, MAVLINK_MSG_ID_RADIO_CALIBRATION_MIN_LEN, MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN, MAVLINK_MSG_ID_RADIO_CALIBRATION_CRC); #else mavlink_radio_calibration_t packet; mav_array_memcpy(packet.aileron, aileron, sizeof(uint16_t)*3); mav_array_memcpy(packet.elevator, elevator, sizeof(uint16_t)*3); mav_array_memcpy(packet.rudder, rudder, sizeof(uint16_t)*3); mav_array_memcpy(packet.gyro, gyro, sizeof(uint16_t)*2); mav_array_memcpy(packet.pitch, pitch, sizeof(uint16_t)*5); mav_array_memcpy(packet.throttle, throttle, sizeof(uint16_t)*5); _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RADIO_CALIBRATION, (const char *)&packet, MAVLINK_MSG_ID_RADIO_CALIBRATION_MIN_LEN, MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN, MAVLINK_MSG_ID_RADIO_CALIBRATION_CRC); #endif } /** * @brief Send a radio_calibration message * @param chan MAVLink channel to send the message * @param struct The MAVLink struct to serialize */ static inline void mavlink_msg_radio_calibration_send_struct(mavlink_channel_t chan, const mavlink_radio_calibration_t* radio_calibration) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS mavlink_msg_radio_calibration_send(chan, radio_calibration->aileron, radio_calibration->elevator, radio_calibration->rudder, radio_calibration->gyro, radio_calibration->pitch, radio_calibration->throttle); #else _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RADIO_CALIBRATION, (const char *)radio_calibration, MAVLINK_MSG_ID_RADIO_CALIBRATION_MIN_LEN, MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN, MAVLINK_MSG_ID_RADIO_CALIBRATION_CRC); #endif } #if MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN <= MAVLINK_MAX_PAYLOAD_LEN /* This variant 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_radio_calibration_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, const uint16_t *aileron, const uint16_t *elevator, const uint16_t *rudder, const uint16_t *gyro, const uint16_t *pitch, const uint16_t *throttle) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char *buf = (char *)msgbuf; _mav_put_uint16_t_array(buf, 0, aileron, 3); _mav_put_uint16_t_array(buf, 6, elevator, 3); _mav_put_uint16_t_array(buf, 12, rudder, 3); _mav_put_uint16_t_array(buf, 18, gyro, 2); _mav_put_uint16_t_array(buf, 22, pitch, 5); _mav_put_uint16_t_array(buf, 32, throttle, 5); _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RADIO_CALIBRATION, buf, MAVLINK_MSG_ID_RADIO_CALIBRATION_MIN_LEN, MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN, MAVLINK_MSG_ID_RADIO_CALIBRATION_CRC); #else mavlink_radio_calibration_t *packet = (mavlink_radio_calibration_t *)msgbuf; mav_array_memcpy(packet->aileron, aileron, sizeof(uint16_t)*3); mav_array_memcpy(packet->elevator, elevator, sizeof(uint16_t)*3); mav_array_memcpy(packet->rudder, rudder, sizeof(uint16_t)*3); mav_array_memcpy(packet->gyro, gyro, sizeof(uint16_t)*2); mav_array_memcpy(packet->pitch, pitch, sizeof(uint16_t)*5); mav_array_memcpy(packet->throttle, throttle, sizeof(uint16_t)*5); _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RADIO_CALIBRATION, (const char *)packet, MAVLINK_MSG_ID_RADIO_CALIBRATION_MIN_LEN, MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN, MAVLINK_MSG_ID_RADIO_CALIBRATION_CRC); #endif } #endif #endif // MESSAGE RADIO_CALIBRATION UNPACKING /** * @brief Get field aileron from radio_calibration message * * @return Aileron setpoints: left, center, right */ static inline uint16_t mavlink_msg_radio_calibration_get_aileron(const mavlink_message_t* msg, uint16_t *aileron) { return _MAV_RETURN_uint16_t_array(msg, aileron, 3, 0); } /** * @brief Get field elevator from radio_calibration message * * @return Elevator setpoints: nose down, center, nose up */ static inline uint16_t mavlink_msg_radio_calibration_get_elevator(const mavlink_message_t* msg, uint16_t *elevator) { return _MAV_RETURN_uint16_t_array(msg, elevator, 3, 6); } /** * @brief Get field rudder from radio_calibration message * * @return Rudder setpoints: nose left, center, nose right */ static inline uint16_t mavlink_msg_radio_calibration_get_rudder(const mavlink_message_t* msg, uint16_t *rudder) { return _MAV_RETURN_uint16_t_array(msg, rudder, 3, 12); } /** * @brief Get field gyro from radio_calibration message * * @return Tail gyro mode/gain setpoints: heading hold, rate mode */ static inline uint16_t mavlink_msg_radio_calibration_get_gyro(const mavlink_message_t* msg, uint16_t *gyro) { return _MAV_RETURN_uint16_t_array(msg, gyro, 2, 18); } /** * @brief Get field pitch from radio_calibration message * * @return Pitch curve setpoints (every 25%) */ static inline uint16_t mavlink_msg_radio_calibration_get_pitch(const mavlink_message_t* msg, uint16_t *pitch) { return _MAV_RETURN_uint16_t_array(msg, pitch, 5, 22); } /** * @brief Get field throttle from radio_calibration message * * @return Throttle curve setpoints (every 25%) */ static inline uint16_t mavlink_msg_radio_calibration_get_throttle(const mavlink_message_t* msg, uint16_t *throttle) { return _MAV_RETURN_uint16_t_array(msg, throttle, 5, 32); } /** * @brief Decode a radio_calibration message into a struct * * @param msg The message to decode * @param radio_calibration C-struct to decode the message contents into */ static inline void mavlink_msg_radio_calibration_decode(const mavlink_message_t* msg, mavlink_radio_calibration_t* radio_calibration) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS mavlink_msg_radio_calibration_get_aileron(msg, radio_calibration->aileron); mavlink_msg_radio_calibration_get_elevator(msg, radio_calibration->elevator); mavlink_msg_radio_calibration_get_rudder(msg, radio_calibration->rudder); mavlink_msg_radio_calibration_get_gyro(msg, radio_calibration->gyro); mavlink_msg_radio_calibration_get_pitch(msg, radio_calibration->pitch); mavlink_msg_radio_calibration_get_throttle(msg, radio_calibration->throttle); #else uint8_t len = msg->len < MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN? msg->len : MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN; memset(radio_calibration, 0, MAVLINK_MSG_ID_RADIO_CALIBRATION_LEN); memcpy(radio_calibration, _MAV_PAYLOAD(msg), len); #endif }