#pragma once // MESSAGE VK_FIXEDWING_CONTROL_VALUE PACKING #define MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE 53009 typedef struct __mavlink_vk_fixedwing_control_value_t { uint32_t timestamp; /*< [ms] Timestamp from system boot.*/ float roll_value; /*< Roll control value, negative value means roll left.*/ float pitch_value; /*< Pitch control value, negative value means pitch down.*/ float throttle_value; /*< Throttle control value, negative value means throttle off*/ float yaw_value; /*< Throttle control value, negative value means turn left*/ } mavlink_vk_fixedwing_control_value_t; #define MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN 20 #define MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN 20 #define MAVLINK_MSG_ID_53009_LEN 20 #define MAVLINK_MSG_ID_53009_MIN_LEN 20 #define MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC 226 #define MAVLINK_MSG_ID_53009_CRC 226 #if MAVLINK_COMMAND_24BIT #define MAVLINK_MESSAGE_INFO_VK_FIXEDWING_CONTROL_VALUE { \ 53009, \ "VK_FIXEDWING_CONTROL_VALUE", \ 5, \ { { "timestamp", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_vk_fixedwing_control_value_t, timestamp) }, \ { "roll_value", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_vk_fixedwing_control_value_t, roll_value) }, \ { "pitch_value", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_vk_fixedwing_control_value_t, pitch_value) }, \ { "throttle_value", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_vk_fixedwing_control_value_t, throttle_value) }, \ { "yaw_value", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_vk_fixedwing_control_value_t, yaw_value) }, \ } \ } #else #define MAVLINK_MESSAGE_INFO_VK_FIXEDWING_CONTROL_VALUE { \ "VK_FIXEDWING_CONTROL_VALUE", \ 5, \ { { "timestamp", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_vk_fixedwing_control_value_t, timestamp) }, \ { "roll_value", NULL, MAVLINK_TYPE_FLOAT, 0, 4, offsetof(mavlink_vk_fixedwing_control_value_t, roll_value) }, \ { "pitch_value", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_vk_fixedwing_control_value_t, pitch_value) }, \ { "throttle_value", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_vk_fixedwing_control_value_t, throttle_value) }, \ { "yaw_value", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_vk_fixedwing_control_value_t, yaw_value) }, \ } \ } #endif /** * @brief Pack a vk_fixedwing_control_value 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 timestamp [ms] Timestamp from system boot. * @param roll_value Roll control value, negative value means roll left. * @param pitch_value Pitch control value, negative value means pitch down. * @param throttle_value Throttle control value, negative value means throttle off * @param yaw_value Throttle control value, negative value means turn left * @return length of the message in bytes (excluding serial stream start sign) */ static inline uint16_t mavlink_msg_vk_fixedwing_control_value_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, uint32_t timestamp, float roll_value, float pitch_value, float throttle_value, float yaw_value) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN]; _mav_put_uint32_t(buf, 0, timestamp); _mav_put_float(buf, 4, roll_value); _mav_put_float(buf, 8, pitch_value); _mav_put_float(buf, 12, throttle_value); _mav_put_float(buf, 16, yaw_value); memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN); #else mavlink_vk_fixedwing_control_value_t packet; packet.timestamp = timestamp; packet.roll_value = roll_value; packet.pitch_value = pitch_value; packet.throttle_value = throttle_value; packet.yaw_value = yaw_value; memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN); #endif msg->msgid = MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE; return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC); } /** * @brief Pack a vk_fixedwing_control_value message * @param system_id ID of this system * @param component_id ID of this component (e.g. 200 for IMU) * @param status MAVLink status structure * @param msg The MAVLink message to compress the data into * * @param timestamp [ms] Timestamp from system boot. * @param roll_value Roll control value, negative value means roll left. * @param pitch_value Pitch control value, negative value means pitch down. * @param throttle_value Throttle control value, negative value means throttle off * @param yaw_value Throttle control value, negative value means turn left * @return length of the message in bytes (excluding serial stream start sign) */ static inline uint16_t mavlink_msg_vk_fixedwing_control_value_pack_status(uint8_t system_id, uint8_t component_id, mavlink_status_t *_status, mavlink_message_t* msg, uint32_t timestamp, float roll_value, float pitch_value, float throttle_value, float yaw_value) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN]; _mav_put_uint32_t(buf, 0, timestamp); _mav_put_float(buf, 4, roll_value); _mav_put_float(buf, 8, pitch_value); _mav_put_float(buf, 12, throttle_value); _mav_put_float(buf, 16, yaw_value); memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN); #else mavlink_vk_fixedwing_control_value_t packet; packet.timestamp = timestamp; packet.roll_value = roll_value; packet.pitch_value = pitch_value; packet.throttle_value = throttle_value; packet.yaw_value = yaw_value; memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN); #endif msg->msgid = MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE; #if MAVLINK_CRC_EXTRA return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC); #else return mavlink_finalize_message_buffer(msg, system_id, component_id, _status, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN); #endif } /** * @brief Pack a vk_fixedwing_control_value 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 timestamp [ms] Timestamp from system boot. * @param roll_value Roll control value, negative value means roll left. * @param pitch_value Pitch control value, negative value means pitch down. * @param throttle_value Throttle control value, negative value means throttle off * @param yaw_value Throttle control value, negative value means turn left * @return length of the message in bytes (excluding serial stream start sign) */ static inline uint16_t mavlink_msg_vk_fixedwing_control_value_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, uint32_t timestamp,float roll_value,float pitch_value,float throttle_value,float yaw_value) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN]; _mav_put_uint32_t(buf, 0, timestamp); _mav_put_float(buf, 4, roll_value); _mav_put_float(buf, 8, pitch_value); _mav_put_float(buf, 12, throttle_value); _mav_put_float(buf, 16, yaw_value); memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN); #else mavlink_vk_fixedwing_control_value_t packet; packet.timestamp = timestamp; packet.roll_value = roll_value; packet.pitch_value = pitch_value; packet.throttle_value = throttle_value; packet.yaw_value = yaw_value; memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN); #endif msg->msgid = MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE; return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC); } /** * @brief Encode a vk_fixedwing_control_value 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 vk_fixedwing_control_value C-struct to read the message contents from */ static inline uint16_t mavlink_msg_vk_fixedwing_control_value_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value) { return mavlink_msg_vk_fixedwing_control_value_pack(system_id, component_id, msg, vk_fixedwing_control_value->timestamp, vk_fixedwing_control_value->roll_value, vk_fixedwing_control_value->pitch_value, vk_fixedwing_control_value->throttle_value, vk_fixedwing_control_value->yaw_value); } /** * @brief Encode a vk_fixedwing_control_value 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 vk_fixedwing_control_value C-struct to read the message contents from */ static inline uint16_t mavlink_msg_vk_fixedwing_control_value_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value) { return mavlink_msg_vk_fixedwing_control_value_pack_chan(system_id, component_id, chan, msg, vk_fixedwing_control_value->timestamp, vk_fixedwing_control_value->roll_value, vk_fixedwing_control_value->pitch_value, vk_fixedwing_control_value->throttle_value, vk_fixedwing_control_value->yaw_value); } /** * @brief Encode a vk_fixedwing_control_value struct with provided status structure * * @param system_id ID of this system * @param component_id ID of this component (e.g. 200 for IMU) * @param status MAVLink status structure * @param msg The MAVLink message to compress the data into * @param vk_fixedwing_control_value C-struct to read the message contents from */ static inline uint16_t mavlink_msg_vk_fixedwing_control_value_encode_status(uint8_t system_id, uint8_t component_id, mavlink_status_t* _status, mavlink_message_t* msg, const mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value) { return mavlink_msg_vk_fixedwing_control_value_pack_status(system_id, component_id, _status, msg, vk_fixedwing_control_value->timestamp, vk_fixedwing_control_value->roll_value, vk_fixedwing_control_value->pitch_value, vk_fixedwing_control_value->throttle_value, vk_fixedwing_control_value->yaw_value); } /** * @brief Send a vk_fixedwing_control_value message * @param chan MAVLink channel to send the message * * @param timestamp [ms] Timestamp from system boot. * @param roll_value Roll control value, negative value means roll left. * @param pitch_value Pitch control value, negative value means pitch down. * @param throttle_value Throttle control value, negative value means throttle off * @param yaw_value Throttle control value, negative value means turn left */ #ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS static inline void mavlink_msg_vk_fixedwing_control_value_send(mavlink_channel_t chan, uint32_t timestamp, float roll_value, float pitch_value, float throttle_value, float yaw_value) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char buf[MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN]; _mav_put_uint32_t(buf, 0, timestamp); _mav_put_float(buf, 4, roll_value); _mav_put_float(buf, 8, pitch_value); _mav_put_float(buf, 12, throttle_value); _mav_put_float(buf, 16, yaw_value); _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC); #else mavlink_vk_fixedwing_control_value_t packet; packet.timestamp = timestamp; packet.roll_value = roll_value; packet.pitch_value = pitch_value; packet.throttle_value = throttle_value; packet.yaw_value = yaw_value; _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, (const char *)&packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC); #endif } /** * @brief Send a vk_fixedwing_control_value message * @param chan MAVLink channel to send the message * @param struct The MAVLink struct to serialize */ static inline void mavlink_msg_vk_fixedwing_control_value_send_struct(mavlink_channel_t chan, const mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS mavlink_msg_vk_fixedwing_control_value_send(chan, vk_fixedwing_control_value->timestamp, vk_fixedwing_control_value->roll_value, vk_fixedwing_control_value->pitch_value, vk_fixedwing_control_value->throttle_value, vk_fixedwing_control_value->yaw_value); #else _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, (const char *)vk_fixedwing_control_value, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC); #endif } #if MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_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_vk_fixedwing_control_value_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_t timestamp, float roll_value, float pitch_value, float throttle_value, float yaw_value) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS char *buf = (char *)msgbuf; _mav_put_uint32_t(buf, 0, timestamp); _mav_put_float(buf, 4, roll_value); _mav_put_float(buf, 8, pitch_value); _mav_put_float(buf, 12, throttle_value); _mav_put_float(buf, 16, yaw_value); _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, buf, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC); #else mavlink_vk_fixedwing_control_value_t *packet = (mavlink_vk_fixedwing_control_value_t *)msgbuf; packet->timestamp = timestamp; packet->roll_value = roll_value; packet->pitch_value = pitch_value; packet->throttle_value = throttle_value; packet->yaw_value = yaw_value; _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE, (const char *)packet, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_MIN_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_CRC); #endif } #endif #endif // MESSAGE VK_FIXEDWING_CONTROL_VALUE UNPACKING /** * @brief Get field timestamp from vk_fixedwing_control_value message * * @return [ms] Timestamp from system boot. */ static inline uint32_t mavlink_msg_vk_fixedwing_control_value_get_timestamp(const mavlink_message_t* msg) { return _MAV_RETURN_uint32_t(msg, 0); } /** * @brief Get field roll_value from vk_fixedwing_control_value message * * @return Roll control value, negative value means roll left. */ static inline float mavlink_msg_vk_fixedwing_control_value_get_roll_value(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 4); } /** * @brief Get field pitch_value from vk_fixedwing_control_value message * * @return Pitch control value, negative value means pitch down. */ static inline float mavlink_msg_vk_fixedwing_control_value_get_pitch_value(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 8); } /** * @brief Get field throttle_value from vk_fixedwing_control_value message * * @return Throttle control value, negative value means throttle off */ static inline float mavlink_msg_vk_fixedwing_control_value_get_throttle_value(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 12); } /** * @brief Get field yaw_value from vk_fixedwing_control_value message * * @return Throttle control value, negative value means turn left */ static inline float mavlink_msg_vk_fixedwing_control_value_get_yaw_value(const mavlink_message_t* msg) { return _MAV_RETURN_float(msg, 16); } /** * @brief Decode a vk_fixedwing_control_value message into a struct * * @param msg The message to decode * @param vk_fixedwing_control_value C-struct to decode the message contents into */ static inline void mavlink_msg_vk_fixedwing_control_value_decode(const mavlink_message_t* msg, mavlink_vk_fixedwing_control_value_t* vk_fixedwing_control_value) { #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS vk_fixedwing_control_value->timestamp = mavlink_msg_vk_fixedwing_control_value_get_timestamp(msg); vk_fixedwing_control_value->roll_value = mavlink_msg_vk_fixedwing_control_value_get_roll_value(msg); vk_fixedwing_control_value->pitch_value = mavlink_msg_vk_fixedwing_control_value_get_pitch_value(msg); vk_fixedwing_control_value->throttle_value = mavlink_msg_vk_fixedwing_control_value_get_throttle_value(msg); vk_fixedwing_control_value->yaw_value = mavlink_msg_vk_fixedwing_control_value_get_yaw_value(msg); #else uint8_t len = msg->len < MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN? msg->len : MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN; memset(vk_fixedwing_control_value, 0, MAVLINK_MSG_ID_VK_FIXEDWING_CONTROL_VALUE_LEN); memcpy(vk_fixedwing_control_value, _MAV_PAYLOAD(msg), len); #endif }