File content as of revision 25:bb5356402687:

// 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_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


/**
 * @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)
{
    uint16_t i = 0;
    msg->msgid = MAVLINK_MSG_ID_RADIO_CALIBRATION;

    i += put_array_by_index((const int8_t*)aileron, sizeof(uint16_t)*3, i, msg->payload); // Aileron setpoints: left, center, right
    i += put_array_by_index((const int8_t*)elevator, sizeof(uint16_t)*3, i, msg->payload); // Elevator setpoints: nose down, center, nose up
    i += put_array_by_index((const int8_t*)rudder, sizeof(uint16_t)*3, i, msg->payload); // Rudder setpoints: nose left, center, nose right
    i += put_array_by_index((const int8_t*)gyro, sizeof(uint16_t)*2, i, msg->payload); // Tail gyro mode/gain setpoints: heading hold, rate mode
    i += put_array_by_index((const int8_t*)pitch, sizeof(uint16_t)*5, i, msg->payload); // Pitch curve setpoints (every 25%)
    i += put_array_by_index((const int8_t*)throttle, sizeof(uint16_t)*5, i, msg->payload); // Throttle curve setpoints (every 25%)

    return mavlink_finalize_message(msg, system_id, component_id, i);
}

/**
 * @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 chan The MAVLink channel this message was 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)
{
    uint16_t i = 0;
    msg->msgid = MAVLINK_MSG_ID_RADIO_CALIBRATION;

    i += put_array_by_index((const int8_t*)aileron, sizeof(uint16_t)*3, i, msg->payload); // Aileron setpoints: left, center, right
    i += put_array_by_index((const int8_t*)elevator, sizeof(uint16_t)*3, i, msg->payload); // Elevator setpoints: nose down, center, nose up
    i += put_array_by_index((const int8_t*)rudder, sizeof(uint16_t)*3, i, msg->payload); // Rudder setpoints: nose left, center, nose right
    i += put_array_by_index((const int8_t*)gyro, sizeof(uint16_t)*2, i, msg->payload); // Tail gyro mode/gain setpoints: heading hold, rate mode
    i += put_array_by_index((const int8_t*)pitch, sizeof(uint16_t)*5, i, msg->payload); // Pitch curve setpoints (every 25%)
    i += put_array_by_index((const int8_t*)throttle, sizeof(uint16_t)*5, i, msg->payload); // Throttle curve setpoints (every 25%)

    return mavlink_finalize_message_chan(msg, system_id, component_id, chan, i);
}

/**
 * @brief Encode a radio_calibration 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 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 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)
{
    mavlink_message_t msg;
    mavlink_msg_radio_calibration_pack_chan(mavlink_system.sysid, mavlink_system.compid, chan, &msg, aileron, elevator, rudder, gyro, pitch, throttle);
    mavlink_send_uart(chan, &msg);
}

#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* r_data)
{

    memcpy(r_data, msg->payload, sizeof(uint16_t)*3);
    return sizeof(uint16_t)*3;
}

/**
 * @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* r_data)
{

    memcpy(r_data, msg->payload+sizeof(uint16_t)*3, sizeof(uint16_t)*3);
    return sizeof(uint16_t)*3;
}

/**
 * @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* r_data)
{

    memcpy(r_data, msg->payload+sizeof(uint16_t)*3+sizeof(uint16_t)*3, sizeof(uint16_t)*3);
    return sizeof(uint16_t)*3;
}

/**
 * @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* r_data)
{

    memcpy(r_data, msg->payload+sizeof(uint16_t)*3+sizeof(uint16_t)*3+sizeof(uint16_t)*3, sizeof(uint16_t)*2);
    return sizeof(uint16_t)*2;
}

/**
 * @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* r_data)
{

    memcpy(r_data, msg->payload+sizeof(uint16_t)*3+sizeof(uint16_t)*3+sizeof(uint16_t)*3+sizeof(uint16_t)*2, sizeof(uint16_t)*5);
    return sizeof(uint16_t)*5;
}

/**
 * @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* r_data)
{

    memcpy(r_data, msg->payload+sizeof(uint16_t)*3+sizeof(uint16_t)*3+sizeof(uint16_t)*3+sizeof(uint16_t)*2+sizeof(uint16_t)*5, sizeof(uint16_t)*5);
    return sizeof(uint16_t)*5;
}

/**
 * @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)
{
    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);
}