#pragma once
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// MESSAGE ORBIT_EXECUTION_STATUS PACKING
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#define MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS 360
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typedef struct __mavlink_orbit_execution_status_t {
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uint64_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.*/
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float radius; /*< [m] Radius of the orbit circle. Positive values orbit clockwise, negative values orbit counter-clockwise.*/
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int32_t x; /*< X coordinate of center point. Coordinate system depends on frame field: local = x position in meters * 1e4, global = latitude in degrees * 1e7.*/
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int32_t y; /*< Y coordinate of center point. Coordinate system depends on frame field: local = x position in meters * 1e4, global = latitude in degrees * 1e7.*/
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float z; /*< [m] Altitude of center point. Coordinate system depends on frame field.*/
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uint8_t frame; /*< The coordinate system of the fields: x, y, z.*/
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} mavlink_orbit_execution_status_t;
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#define MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN 25
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#define MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_MIN_LEN 25
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#define MAVLINK_MSG_ID_360_LEN 25
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#define MAVLINK_MSG_ID_360_MIN_LEN 25
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#define MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_CRC 11
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#define MAVLINK_MSG_ID_360_CRC 11
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#if MAVLINK_COMMAND_24BIT
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#define MAVLINK_MESSAGE_INFO_ORBIT_EXECUTION_STATUS { \
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360, \
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"ORBIT_EXECUTION_STATUS", \
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6, \
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{ { "time_usec", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_orbit_execution_status_t, time_usec) }, \
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{ "radius", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_orbit_execution_status_t, radius) }, \
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{ "frame", NULL, MAVLINK_TYPE_UINT8_T, 0, 24, offsetof(mavlink_orbit_execution_status_t, frame) }, \
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{ "x", NULL, MAVLINK_TYPE_INT32_T, 0, 12, offsetof(mavlink_orbit_execution_status_t, x) }, \
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{ "y", NULL, MAVLINK_TYPE_INT32_T, 0, 16, offsetof(mavlink_orbit_execution_status_t, y) }, \
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{ "z", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_orbit_execution_status_t, z) }, \
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} \
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}
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#else
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#define MAVLINK_MESSAGE_INFO_ORBIT_EXECUTION_STATUS { \
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"ORBIT_EXECUTION_STATUS", \
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6, \
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{ { "time_usec", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_orbit_execution_status_t, time_usec) }, \
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{ "radius", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_orbit_execution_status_t, radius) }, \
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{ "frame", NULL, MAVLINK_TYPE_UINT8_T, 0, 24, offsetof(mavlink_orbit_execution_status_t, frame) }, \
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{ "x", NULL, MAVLINK_TYPE_INT32_T, 0, 12, offsetof(mavlink_orbit_execution_status_t, x) }, \
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{ "y", NULL, MAVLINK_TYPE_INT32_T, 0, 16, offsetof(mavlink_orbit_execution_status_t, y) }, \
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{ "z", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_orbit_execution_status_t, z) }, \
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} \
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}
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#endif
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/**
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* @brief Pack a orbit_execution_status message
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* @param system_id ID of this system
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* @param component_id ID of this component (e.g. 200 for IMU)
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* @param msg The MAVLink message to compress the data into
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*
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* @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.
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* @param radius [m] Radius of the orbit circle. Positive values orbit clockwise, negative values orbit counter-clockwise.
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* @param frame The coordinate system of the fields: x, y, z.
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* @param x X coordinate of center point. Coordinate system depends on frame field: local = x position in meters * 1e4, global = latitude in degrees * 1e7.
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* @param y Y coordinate of center point. Coordinate system depends on frame field: local = x position in meters * 1e4, global = latitude in degrees * 1e7.
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* @param z [m] Altitude of center point. Coordinate system depends on frame field.
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* @return length of the message in bytes (excluding serial stream start sign)
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*/
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static inline uint16_t mavlink_msg_orbit_execution_status_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
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uint64_t time_usec, float radius, uint8_t frame, int32_t x, int32_t y, float z)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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char buf[MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN];
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_mav_put_uint64_t(buf, 0, time_usec);
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_mav_put_float(buf, 8, radius);
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_mav_put_int32_t(buf, 12, x);
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_mav_put_int32_t(buf, 16, y);
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_mav_put_float(buf, 20, z);
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_mav_put_uint8_t(buf, 24, frame);
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN);
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#else
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mavlink_orbit_execution_status_t packet;
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packet.time_usec = time_usec;
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packet.radius = radius;
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packet.x = x;
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packet.y = y;
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packet.z = z;
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packet.frame = frame;
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN);
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#endif
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msg->msgid = MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS;
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return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_MIN_LEN, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_CRC);
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}
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/**
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* @brief Pack a orbit_execution_status message on a channel
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* @param system_id ID of this system
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* @param component_id ID of this component (e.g. 200 for IMU)
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* @param chan The MAVLink channel this message will be sent over
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* @param msg The MAVLink message to compress the data into
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* @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.
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* @param radius [m] Radius of the orbit circle. Positive values orbit clockwise, negative values orbit counter-clockwise.
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* @param frame The coordinate system of the fields: x, y, z.
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* @param x X coordinate of center point. Coordinate system depends on frame field: local = x position in meters * 1e4, global = latitude in degrees * 1e7.
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* @param y Y coordinate of center point. Coordinate system depends on frame field: local = x position in meters * 1e4, global = latitude in degrees * 1e7.
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* @param z [m] Altitude of center point. Coordinate system depends on frame field.
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* @return length of the message in bytes (excluding serial stream start sign)
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*/
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static inline uint16_t mavlink_msg_orbit_execution_status_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
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mavlink_message_t* msg,
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uint64_t time_usec,float radius,uint8_t frame,int32_t x,int32_t y,float z)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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char buf[MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN];
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_mav_put_uint64_t(buf, 0, time_usec);
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_mav_put_float(buf, 8, radius);
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_mav_put_int32_t(buf, 12, x);
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_mav_put_int32_t(buf, 16, y);
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_mav_put_float(buf, 20, z);
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_mav_put_uint8_t(buf, 24, frame);
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN);
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#else
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mavlink_orbit_execution_status_t packet;
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packet.time_usec = time_usec;
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packet.radius = radius;
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packet.x = x;
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packet.y = y;
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packet.z = z;
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packet.frame = frame;
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memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN);
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#endif
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msg->msgid = MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS;
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return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_MIN_LEN, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_CRC);
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}
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/**
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* @brief Encode a orbit_execution_status struct
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*
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* @param system_id ID of this system
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* @param component_id ID of this component (e.g. 200 for IMU)
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* @param msg The MAVLink message to compress the data into
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* @param orbit_execution_status C-struct to read the message contents from
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*/
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static inline uint16_t mavlink_msg_orbit_execution_status_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_orbit_execution_status_t* orbit_execution_status)
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{
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return mavlink_msg_orbit_execution_status_pack(system_id, component_id, msg, orbit_execution_status->time_usec, orbit_execution_status->radius, orbit_execution_status->frame, orbit_execution_status->x, orbit_execution_status->y, orbit_execution_status->z);
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}
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/**
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* @brief Encode a orbit_execution_status struct on a channel
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*
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* @param system_id ID of this system
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* @param component_id ID of this component (e.g. 200 for IMU)
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* @param chan The MAVLink channel this message will be sent over
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* @param msg The MAVLink message to compress the data into
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* @param orbit_execution_status C-struct to read the message contents from
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*/
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static inline uint16_t mavlink_msg_orbit_execution_status_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_orbit_execution_status_t* orbit_execution_status)
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{
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return mavlink_msg_orbit_execution_status_pack_chan(system_id, component_id, chan, msg, orbit_execution_status->time_usec, orbit_execution_status->radius, orbit_execution_status->frame, orbit_execution_status->x, orbit_execution_status->y, orbit_execution_status->z);
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}
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/**
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* @brief Send a orbit_execution_status message
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* @param chan MAVLink channel to send the message
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*
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* @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.
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* @param radius [m] Radius of the orbit circle. Positive values orbit clockwise, negative values orbit counter-clockwise.
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* @param frame The coordinate system of the fields: x, y, z.
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* @param x X coordinate of center point. Coordinate system depends on frame field: local = x position in meters * 1e4, global = latitude in degrees * 1e7.
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* @param y Y coordinate of center point. Coordinate system depends on frame field: local = x position in meters * 1e4, global = latitude in degrees * 1e7.
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* @param z [m] Altitude of center point. Coordinate system depends on frame field.
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*/
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#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
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static inline void mavlink_msg_orbit_execution_status_send(mavlink_channel_t chan, uint64_t time_usec, float radius, uint8_t frame, int32_t x, int32_t y, float z)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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char buf[MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN];
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_mav_put_uint64_t(buf, 0, time_usec);
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_mav_put_float(buf, 8, radius);
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_mav_put_int32_t(buf, 12, x);
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_mav_put_int32_t(buf, 16, y);
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_mav_put_float(buf, 20, z);
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_mav_put_uint8_t(buf, 24, frame);
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_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS, buf, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_MIN_LEN, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_CRC);
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#else
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mavlink_orbit_execution_status_t packet;
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packet.time_usec = time_usec;
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packet.radius = radius;
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packet.x = x;
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packet.y = y;
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packet.z = z;
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packet.frame = frame;
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_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS, (const char *)&packet, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_MIN_LEN, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_CRC);
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#endif
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}
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/**
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* @brief Send a orbit_execution_status message
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* @param chan MAVLink channel to send the message
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* @param struct The MAVLink struct to serialize
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*/
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static inline void mavlink_msg_orbit_execution_status_send_struct(mavlink_channel_t chan, const mavlink_orbit_execution_status_t* orbit_execution_status)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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mavlink_msg_orbit_execution_status_send(chan, orbit_execution_status->time_usec, orbit_execution_status->radius, orbit_execution_status->frame, orbit_execution_status->x, orbit_execution_status->y, orbit_execution_status->z);
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#else
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_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS, (const char *)orbit_execution_status, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_MIN_LEN, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_CRC);
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#endif
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}
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#if MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN <= MAVLINK_MAX_PAYLOAD_LEN
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/*
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This variant of _send() can be used to save stack space by re-using
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memory from the receive buffer. The caller provides a
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mavlink_message_t which is the size of a full mavlink message. This
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is usually the receive buffer for the channel, and allows a reply to an
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incoming message with minimum stack space usage.
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*/
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static inline void mavlink_msg_orbit_execution_status_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, float radius, uint8_t frame, int32_t x, int32_t y, float z)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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char *buf = (char *)msgbuf;
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_mav_put_uint64_t(buf, 0, time_usec);
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_mav_put_float(buf, 8, radius);
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_mav_put_int32_t(buf, 12, x);
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_mav_put_int32_t(buf, 16, y);
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_mav_put_float(buf, 20, z);
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_mav_put_uint8_t(buf, 24, frame);
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_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS, buf, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_MIN_LEN, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_CRC);
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#else
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mavlink_orbit_execution_status_t *packet = (mavlink_orbit_execution_status_t *)msgbuf;
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packet->time_usec = time_usec;
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packet->radius = radius;
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packet->x = x;
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packet->y = y;
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packet->z = z;
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packet->frame = frame;
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_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS, (const char *)packet, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_MIN_LEN, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_CRC);
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#endif
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}
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#endif
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#endif
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// MESSAGE ORBIT_EXECUTION_STATUS UNPACKING
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/**
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* @brief Get field time_usec from orbit_execution_status message
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*
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* @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.
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*/
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static inline uint64_t mavlink_msg_orbit_execution_status_get_time_usec(const mavlink_message_t* msg)
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{
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return _MAV_RETURN_uint64_t(msg, 0);
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}
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/**
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* @brief Get field radius from orbit_execution_status message
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*
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* @return [m] Radius of the orbit circle. Positive values orbit clockwise, negative values orbit counter-clockwise.
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*/
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static inline float mavlink_msg_orbit_execution_status_get_radius(const mavlink_message_t* msg)
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{
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return _MAV_RETURN_float(msg, 8);
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}
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/**
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* @brief Get field frame from orbit_execution_status message
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*
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* @return The coordinate system of the fields: x, y, z.
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*/
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static inline uint8_t mavlink_msg_orbit_execution_status_get_frame(const mavlink_message_t* msg)
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{
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return _MAV_RETURN_uint8_t(msg, 24);
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}
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/**
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* @brief Get field x from orbit_execution_status message
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*
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* @return X coordinate of center point. Coordinate system depends on frame field: local = x position in meters * 1e4, global = latitude in degrees * 1e7.
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*/
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static inline int32_t mavlink_msg_orbit_execution_status_get_x(const mavlink_message_t* msg)
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{
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return _MAV_RETURN_int32_t(msg, 12);
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}
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/**
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* @brief Get field y from orbit_execution_status message
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*
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* @return Y coordinate of center point. Coordinate system depends on frame field: local = x position in meters * 1e4, global = latitude in degrees * 1e7.
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*/
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static inline int32_t mavlink_msg_orbit_execution_status_get_y(const mavlink_message_t* msg)
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{
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return _MAV_RETURN_int32_t(msg, 16);
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}
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/**
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* @brief Get field z from orbit_execution_status message
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*
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* @return [m] Altitude of center point. Coordinate system depends on frame field.
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*/
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static inline float mavlink_msg_orbit_execution_status_get_z(const mavlink_message_t* msg)
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{
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return _MAV_RETURN_float(msg, 20);
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}
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/**
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* @brief Decode a orbit_execution_status message into a struct
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*
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* @param msg The message to decode
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* @param orbit_execution_status C-struct to decode the message contents into
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*/
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static inline void mavlink_msg_orbit_execution_status_decode(const mavlink_message_t* msg, mavlink_orbit_execution_status_t* orbit_execution_status)
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{
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#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
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orbit_execution_status->time_usec = mavlink_msg_orbit_execution_status_get_time_usec(msg);
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orbit_execution_status->radius = mavlink_msg_orbit_execution_status_get_radius(msg);
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orbit_execution_status->x = mavlink_msg_orbit_execution_status_get_x(msg);
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orbit_execution_status->y = mavlink_msg_orbit_execution_status_get_y(msg);
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orbit_execution_status->z = mavlink_msg_orbit_execution_status_get_z(msg);
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orbit_execution_status->frame = mavlink_msg_orbit_execution_status_get_frame(msg);
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#else
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uint8_t len = msg->len < MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN? msg->len : MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN;
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memset(orbit_execution_status, 0, MAVLINK_MSG_ID_ORBIT_EXECUTION_STATUS_LEN);
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memcpy(orbit_execution_status, _MAV_PAYLOAD(msg), len);
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#endif
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}
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