mavlink_msg_control_system_state.h

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// MESSAGE CONTROL_SYSTEM_STATE PACKING

#define MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE 146

typedef struct __mavlink_control_system_state_t
{
 uint64_t time_usec; /*< Timestamp (micros since boot or Unix epoch)*/
 float x_acc; /*< X acceleration in body frame*/
 float y_acc; /*< Y acceleration in body frame*/
 float z_acc; /*< Z acceleration in body frame*/
 float x_vel; /*< X velocity in body frame*/
 float y_vel; /*< Y velocity in body frame*/
 float z_vel; /*< Z velocity in body frame*/
 float x_pos; /*< X position in local frame*/
 float y_pos; /*< Y position in local frame*/
 float z_pos; /*< Z position in local frame*/
 float airspeed; /*< Airspeed, set to -1 if unknown*/
 float vel_variance[3]; /*< Variance of body velocity estimate*/
 float pos_variance[3]; /*< Variance in local position*/
 float q[4]; /*< The attitude, represented as Quaternion*/
 float roll_rate; /*< Angular rate in roll axis*/
 float pitch_rate; /*< Angular rate in pitch axis*/
 float yaw_rate; /*< Angular rate in yaw axis*/
} mavlink_control_system_state_t;

#define MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN 100
#define MAVLINK_MSG_ID_146_LEN 100

#define MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_CRC 103
#define MAVLINK_MSG_ID_146_CRC 103

#define MAVLINK_MSG_CONTROL_SYSTEM_STATE_FIELD_VEL_VARIANCE_LEN 3
#define MAVLINK_MSG_CONTROL_SYSTEM_STATE_FIELD_POS_VARIANCE_LEN 3
#define MAVLINK_MSG_CONTROL_SYSTEM_STATE_FIELD_Q_LEN 4

#define MAVLINK_MESSAGE_INFO_CONTROL_SYSTEM_STATE { \
        "CONTROL_SYSTEM_STATE", \
        17, \
        {  { "time_usec", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_control_system_state_t, time_usec) }, \
         { "x_acc", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_control_system_state_t, x_acc) }, \
         { "y_acc", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_control_system_state_t, y_acc) }, \
         { "z_acc", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_control_system_state_t, z_acc) }, \
         { "x_vel", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_control_system_state_t, x_vel) }, \
         { "y_vel", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_control_system_state_t, y_vel) }, \
         { "z_vel", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_control_system_state_t, z_vel) }, \
         { "x_pos", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_control_system_state_t, x_pos) }, \
         { "y_pos", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_control_system_state_t, y_pos) }, \
         { "z_pos", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_control_system_state_t, z_pos) }, \
         { "airspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_control_system_state_t, airspeed) }, \
         { "vel_variance", NULL, MAVLINK_TYPE_FLOAT, 3, 48, offsetof(mavlink_control_system_state_t, vel_variance) }, \
         { "pos_variance", NULL, MAVLINK_TYPE_FLOAT, 3, 60, offsetof(mavlink_control_system_state_t, pos_variance) }, \
         { "q", NULL, MAVLINK_TYPE_FLOAT, 4, 72, offsetof(mavlink_control_system_state_t, q) }, \
         { "roll_rate", NULL, MAVLINK_TYPE_FLOAT, 0, 88, offsetof(mavlink_control_system_state_t, roll_rate) }, \
         { "pitch_rate", NULL, MAVLINK_TYPE_FLOAT, 0, 92, offsetof(mavlink_control_system_state_t, pitch_rate) }, \
         { "yaw_rate", NULL, MAVLINK_TYPE_FLOAT, 0, 96, offsetof(mavlink_control_system_state_t, yaw_rate) }, \
         } \
}


static inline uint16_t mavlink_msg_control_system_state_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
                                                       uint64_t time_usec, float x_acc, float y_acc, float z_acc, float x_vel, float y_vel, float z_vel, float x_pos, float y_pos, float z_pos, float airspeed, const float *vel_variance, const float *pos_variance, const float *q, float roll_rate, float pitch_rate, float yaw_rate)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
        char buf[MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN];
        _mav_put_uint64_t(buf, 0, time_usec);
        _mav_put_float(buf, 8, x_acc);
        _mav_put_float(buf, 12, y_acc);
        _mav_put_float(buf, 16, z_acc);
        _mav_put_float(buf, 20, x_vel);
        _mav_put_float(buf, 24, y_vel);
        _mav_put_float(buf, 28, z_vel);
        _mav_put_float(buf, 32, x_pos);
        _mav_put_float(buf, 36, y_pos);
        _mav_put_float(buf, 40, z_pos);
        _mav_put_float(buf, 44, airspeed);
        _mav_put_float(buf, 88, roll_rate);
        _mav_put_float(buf, 92, pitch_rate);
        _mav_put_float(buf, 96, yaw_rate);
        _mav_put_float_array(buf, 48, vel_variance, 3);
        _mav_put_float_array(buf, 60, pos_variance, 3);
        _mav_put_float_array(buf, 72, q, 4);
        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN);
#else
        mavlink_control_system_state_t packet;
        packet.time_usec = time_usec;
        packet.x_acc = x_acc;
        packet.y_acc = y_acc;
        packet.z_acc = z_acc;
        packet.x_vel = x_vel;
        packet.y_vel = y_vel;
        packet.z_vel = z_vel;
        packet.x_pos = x_pos;
        packet.y_pos = y_pos;
        packet.z_pos = z_pos;
        packet.airspeed = airspeed;
        packet.roll_rate = roll_rate;
        packet.pitch_rate = pitch_rate;
        packet.yaw_rate = yaw_rate;
        mav_array_memcpy(packet.vel_variance, vel_variance, sizeof(float)*3);
        mav_array_memcpy(packet.pos_variance, pos_variance, sizeof(float)*3);
        mav_array_memcpy(packet.q, q, sizeof(float)*4);
        memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN);
#endif

        msg->msgid = MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE;
#if MAVLINK_CRC_EXTRA
    return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_CRC);
#else
    return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN);
#endif
}

static inline uint16_t mavlink_msg_control_system_state_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
                                                           mavlink_message_t* msg,
                                                           uint64_t time_usec,float x_acc,float y_acc,float z_acc,float x_vel,float y_vel,float z_vel,float x_pos,float y_pos,float z_pos,float airspeed,const float *vel_variance,const float *pos_variance,const float *q,float roll_rate,float pitch_rate,float yaw_rate)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
        char buf[MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN];
        _mav_put_uint64_t(buf, 0, time_usec);
        _mav_put_float(buf, 8, x_acc);
        _mav_put_float(buf, 12, y_acc);
        _mav_put_float(buf, 16, z_acc);
        _mav_put_float(buf, 20, x_vel);
        _mav_put_float(buf, 24, y_vel);
        _mav_put_float(buf, 28, z_vel);
        _mav_put_float(buf, 32, x_pos);
        _mav_put_float(buf, 36, y_pos);
        _mav_put_float(buf, 40, z_pos);
        _mav_put_float(buf, 44, airspeed);
        _mav_put_float(buf, 88, roll_rate);
        _mav_put_float(buf, 92, pitch_rate);
        _mav_put_float(buf, 96, yaw_rate);
        _mav_put_float_array(buf, 48, vel_variance, 3);
        _mav_put_float_array(buf, 60, pos_variance, 3);
        _mav_put_float_array(buf, 72, q, 4);
        memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN);
#else
        mavlink_control_system_state_t packet;
        packet.time_usec = time_usec;
        packet.x_acc = x_acc;
        packet.y_acc = y_acc;
        packet.z_acc = z_acc;
        packet.x_vel = x_vel;
        packet.y_vel = y_vel;
        packet.z_vel = z_vel;
        packet.x_pos = x_pos;
        packet.y_pos = y_pos;
        packet.z_pos = z_pos;
        packet.airspeed = airspeed;
        packet.roll_rate = roll_rate;
        packet.pitch_rate = pitch_rate;
        packet.yaw_rate = yaw_rate;
        mav_array_memcpy(packet.vel_variance, vel_variance, sizeof(float)*3);
        mav_array_memcpy(packet.pos_variance, pos_variance, sizeof(float)*3);
        mav_array_memcpy(packet.q, q, sizeof(float)*4);
        memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN);
#endif

        msg->msgid = MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE;
#if MAVLINK_CRC_EXTRA
    return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_CRC);
#else
    return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN);
#endif
}

static inline uint16_t mavlink_msg_control_system_state_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_control_system_state_t* control_system_state)
{
        return mavlink_msg_control_system_state_pack(system_id, component_id, msg, control_system_state->time_usec, control_system_state->x_acc, control_system_state->y_acc, control_system_state->z_acc, control_system_state->x_vel, control_system_state->y_vel, control_system_state->z_vel, control_system_state->x_pos, control_system_state->y_pos, control_system_state->z_pos, control_system_state->airspeed, control_system_state->vel_variance, control_system_state->pos_variance, control_system_state->q, control_system_state->roll_rate, control_system_state->pitch_rate, control_system_state->yaw_rate);
}

static inline uint16_t mavlink_msg_control_system_state_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_control_system_state_t* control_system_state)
{
        return mavlink_msg_control_system_state_pack_chan(system_id, component_id, chan, msg, control_system_state->time_usec, control_system_state->x_acc, control_system_state->y_acc, control_system_state->z_acc, control_system_state->x_vel, control_system_state->y_vel, control_system_state->z_vel, control_system_state->x_pos, control_system_state->y_pos, control_system_state->z_pos, control_system_state->airspeed, control_system_state->vel_variance, control_system_state->pos_variance, control_system_state->q, control_system_state->roll_rate, control_system_state->pitch_rate, control_system_state->yaw_rate);
}

#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS

static inline void mavlink_msg_control_system_state_send(mavlink_channel_t chan, uint64_t time_usec, float x_acc, float y_acc, float z_acc, float x_vel, float y_vel, float z_vel, float x_pos, float y_pos, float z_pos, float airspeed, const float *vel_variance, const float *pos_variance, const float *q, float roll_rate, float pitch_rate, float yaw_rate)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
        char buf[MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN];
        _mav_put_uint64_t(buf, 0, time_usec);
        _mav_put_float(buf, 8, x_acc);
        _mav_put_float(buf, 12, y_acc);
        _mav_put_float(buf, 16, z_acc);
        _mav_put_float(buf, 20, x_vel);
        _mav_put_float(buf, 24, y_vel);
        _mav_put_float(buf, 28, z_vel);
        _mav_put_float(buf, 32, x_pos);
        _mav_put_float(buf, 36, y_pos);
        _mav_put_float(buf, 40, z_pos);
        _mav_put_float(buf, 44, airspeed);
        _mav_put_float(buf, 88, roll_rate);
        _mav_put_float(buf, 92, pitch_rate);
        _mav_put_float(buf, 96, yaw_rate);
        _mav_put_float_array(buf, 48, vel_variance, 3);
        _mav_put_float_array(buf, 60, pos_variance, 3);
        _mav_put_float_array(buf, 72, q, 4);
#if MAVLINK_CRC_EXTRA
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE, buf, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_CRC);
#else
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE, buf, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN);
#endif
#else
        mavlink_control_system_state_t packet;
        packet.time_usec = time_usec;
        packet.x_acc = x_acc;
        packet.y_acc = y_acc;
        packet.z_acc = z_acc;
        packet.x_vel = x_vel;
        packet.y_vel = y_vel;
        packet.z_vel = z_vel;
        packet.x_pos = x_pos;
        packet.y_pos = y_pos;
        packet.z_pos = z_pos;
        packet.airspeed = airspeed;
        packet.roll_rate = roll_rate;
        packet.pitch_rate = pitch_rate;
        packet.yaw_rate = yaw_rate;
        mav_array_memcpy(packet.vel_variance, vel_variance, sizeof(float)*3);
        mav_array_memcpy(packet.pos_variance, pos_variance, sizeof(float)*3);
        mav_array_memcpy(packet.q, q, sizeof(float)*4);
#if MAVLINK_CRC_EXTRA
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE, (const char *)&packet, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_CRC);
#else
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE, (const char *)&packet, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN);
#endif
#endif
}

#if MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN <= MAVLINK_MAX_PAYLOAD_LEN
/*
  This varient 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_control_system_state_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan,  uint64_t time_usec, float x_acc, float y_acc, float z_acc, float x_vel, float y_vel, float z_vel, float x_pos, float y_pos, float z_pos, float airspeed, const float *vel_variance, const float *pos_variance, const float *q, float roll_rate, float pitch_rate, float yaw_rate)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
        char *buf = (char *)msgbuf;
        _mav_put_uint64_t(buf, 0, time_usec);
        _mav_put_float(buf, 8, x_acc);
        _mav_put_float(buf, 12, y_acc);
        _mav_put_float(buf, 16, z_acc);
        _mav_put_float(buf, 20, x_vel);
        _mav_put_float(buf, 24, y_vel);
        _mav_put_float(buf, 28, z_vel);
        _mav_put_float(buf, 32, x_pos);
        _mav_put_float(buf, 36, y_pos);
        _mav_put_float(buf, 40, z_pos);
        _mav_put_float(buf, 44, airspeed);
        _mav_put_float(buf, 88, roll_rate);
        _mav_put_float(buf, 92, pitch_rate);
        _mav_put_float(buf, 96, yaw_rate);
        _mav_put_float_array(buf, 48, vel_variance, 3);
        _mav_put_float_array(buf, 60, pos_variance, 3);
        _mav_put_float_array(buf, 72, q, 4);
#if MAVLINK_CRC_EXTRA
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE, buf, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_CRC);
#else
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE, buf, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN);
#endif
#else
        mavlink_control_system_state_t *packet = (mavlink_control_system_state_t *)msgbuf;
        packet->time_usec = time_usec;
        packet->x_acc = x_acc;
        packet->y_acc = y_acc;
        packet->z_acc = z_acc;
        packet->x_vel = x_vel;
        packet->y_vel = y_vel;
        packet->z_vel = z_vel;
        packet->x_pos = x_pos;
        packet->y_pos = y_pos;
        packet->z_pos = z_pos;
        packet->airspeed = airspeed;
        packet->roll_rate = roll_rate;
        packet->pitch_rate = pitch_rate;
        packet->yaw_rate = yaw_rate;
        mav_array_memcpy(packet->vel_variance, vel_variance, sizeof(float)*3);
        mav_array_memcpy(packet->pos_variance, pos_variance, sizeof(float)*3);
        mav_array_memcpy(packet->q, q, sizeof(float)*4);
#if MAVLINK_CRC_EXTRA
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE, (const char *)packet, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_CRC);
#else
    _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE, (const char *)packet, MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN);
#endif
#endif
}
#endif

#endif

// MESSAGE CONTROL_SYSTEM_STATE UNPACKING


static inline uint64_t mavlink_msg_control_system_state_get_time_usec(const mavlink_message_t* msg)
{
        return _MAV_RETURN_uint64_t(msg,  0);
}

static inline float mavlink_msg_control_system_state_get_x_acc(const mavlink_message_t* msg)
{
        return _MAV_RETURN_float(msg,  8);
}

static inline float mavlink_msg_control_system_state_get_y_acc(const mavlink_message_t* msg)
{
        return _MAV_RETURN_float(msg,  12);
}

static inline float mavlink_msg_control_system_state_get_z_acc(const mavlink_message_t* msg)
{
        return _MAV_RETURN_float(msg,  16);
}

static inline float mavlink_msg_control_system_state_get_x_vel(const mavlink_message_t* msg)
{
        return _MAV_RETURN_float(msg,  20);
}

static inline float mavlink_msg_control_system_state_get_y_vel(const mavlink_message_t* msg)
{
        return _MAV_RETURN_float(msg,  24);
}

static inline float mavlink_msg_control_system_state_get_z_vel(const mavlink_message_t* msg)
{
        return _MAV_RETURN_float(msg,  28);
}

static inline float mavlink_msg_control_system_state_get_x_pos(const mavlink_message_t* msg)
{
        return _MAV_RETURN_float(msg,  32);
}

static inline float mavlink_msg_control_system_state_get_y_pos(const mavlink_message_t* msg)
{
        return _MAV_RETURN_float(msg,  36);
}

static inline float mavlink_msg_control_system_state_get_z_pos(const mavlink_message_t* msg)
{
        return _MAV_RETURN_float(msg,  40);
}

static inline float mavlink_msg_control_system_state_get_airspeed(const mavlink_message_t* msg)
{
        return _MAV_RETURN_float(msg,  44);
}

static inline uint16_t mavlink_msg_control_system_state_get_vel_variance(const mavlink_message_t* msg, float *vel_variance)
{
        return _MAV_RETURN_float_array(msg, vel_variance, 3,  48);
}

static inline uint16_t mavlink_msg_control_system_state_get_pos_variance(const mavlink_message_t* msg, float *pos_variance)
{
        return _MAV_RETURN_float_array(msg, pos_variance, 3,  60);
}

static inline uint16_t mavlink_msg_control_system_state_get_q(const mavlink_message_t* msg, float *q)
{
        return _MAV_RETURN_float_array(msg, q, 4,  72);
}

static inline float mavlink_msg_control_system_state_get_roll_rate(const mavlink_message_t* msg)
{
        return _MAV_RETURN_float(msg,  88);
}

static inline float mavlink_msg_control_system_state_get_pitch_rate(const mavlink_message_t* msg)
{
        return _MAV_RETURN_float(msg,  92);
}

static inline float mavlink_msg_control_system_state_get_yaw_rate(const mavlink_message_t* msg)
{
        return _MAV_RETURN_float(msg,  96);
}

static inline void mavlink_msg_control_system_state_decode(const mavlink_message_t* msg, mavlink_control_system_state_t* control_system_state)
{
#if MAVLINK_NEED_BYTE_SWAP
        control_system_state->time_usec = mavlink_msg_control_system_state_get_time_usec(msg);
        control_system_state->x_acc = mavlink_msg_control_system_state_get_x_acc(msg);
        control_system_state->y_acc = mavlink_msg_control_system_state_get_y_acc(msg);
        control_system_state->z_acc = mavlink_msg_control_system_state_get_z_acc(msg);
        control_system_state->x_vel = mavlink_msg_control_system_state_get_x_vel(msg);
        control_system_state->y_vel = mavlink_msg_control_system_state_get_y_vel(msg);
        control_system_state->z_vel = mavlink_msg_control_system_state_get_z_vel(msg);
        control_system_state->x_pos = mavlink_msg_control_system_state_get_x_pos(msg);
        control_system_state->y_pos = mavlink_msg_control_system_state_get_y_pos(msg);
        control_system_state->z_pos = mavlink_msg_control_system_state_get_z_pos(msg);
        control_system_state->airspeed = mavlink_msg_control_system_state_get_airspeed(msg);
        mavlink_msg_control_system_state_get_vel_variance(msg, control_system_state->vel_variance);
        mavlink_msg_control_system_state_get_pos_variance(msg, control_system_state->pos_variance);
        mavlink_msg_control_system_state_get_q(msg, control_system_state->q);
        control_system_state->roll_rate = mavlink_msg_control_system_state_get_roll_rate(msg);
        control_system_state->pitch_rate = mavlink_msg_control_system_state_get_pitch_rate(msg);
        control_system_state->yaw_rate = mavlink_msg_control_system_state_get_yaw_rate(msg);
#else
        memcpy(control_system_state, _MAV_PAYLOAD(msg), MAVLINK_MSG_ID_CONTROL_SYSTEM_STATE_LEN);
#endif
}