00001
00002
00003 #define MAVLINK_MSG_ID_HIL_STATE_QUATERNION 115
00004
00005 typedef struct __mavlink_hil_state_quaternion_t
00006 {
00007 uint64_t time_usec;
00008 float attitude_quaternion[4];
00009 float rollspeed;
00010 float pitchspeed;
00011 float yawspeed;
00012 int32_t lat;
00013 int32_t lon;
00014 int32_t alt;
00015 int16_t vx;
00016 int16_t vy;
00017 int16_t vz;
00018 uint16_t ind_airspeed;
00019 uint16_t true_airspeed;
00020 int16_t xacc;
00021 int16_t yacc;
00022 int16_t zacc;
00023 } mavlink_hil_state_quaternion_t;
00024
00025 #define MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN 64
00026 #define MAVLINK_MSG_ID_115_LEN 64
00027
00028 #define MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC 4
00029 #define MAVLINK_MSG_ID_115_CRC 4
00030
00031 #define MAVLINK_MSG_HIL_STATE_QUATERNION_FIELD_ATTITUDE_QUATERNION_LEN 4
00032
00033 #define MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION { \
00034 "HIL_STATE_QUATERNION", \
00035 16, \
00036 { { "time_usec", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_hil_state_quaternion_t, time_usec) }, \
00037 { "attitude_quaternion", NULL, MAVLINK_TYPE_FLOAT, 4, 8, offsetof(mavlink_hil_state_quaternion_t, attitude_quaternion) }, \
00038 { "rollspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_hil_state_quaternion_t, rollspeed) }, \
00039 { "pitchspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_hil_state_quaternion_t, pitchspeed) }, \
00040 { "yawspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_hil_state_quaternion_t, yawspeed) }, \
00041 { "lat", NULL, MAVLINK_TYPE_INT32_T, 0, 36, offsetof(mavlink_hil_state_quaternion_t, lat) }, \
00042 { "lon", NULL, MAVLINK_TYPE_INT32_T, 0, 40, offsetof(mavlink_hil_state_quaternion_t, lon) }, \
00043 { "alt", NULL, MAVLINK_TYPE_INT32_T, 0, 44, offsetof(mavlink_hil_state_quaternion_t, alt) }, \
00044 { "vx", NULL, MAVLINK_TYPE_INT16_T, 0, 48, offsetof(mavlink_hil_state_quaternion_t, vx) }, \
00045 { "vy", NULL, MAVLINK_TYPE_INT16_T, 0, 50, offsetof(mavlink_hil_state_quaternion_t, vy) }, \
00046 { "vz", NULL, MAVLINK_TYPE_INT16_T, 0, 52, offsetof(mavlink_hil_state_quaternion_t, vz) }, \
00047 { "ind_airspeed", NULL, MAVLINK_TYPE_UINT16_T, 0, 54, offsetof(mavlink_hil_state_quaternion_t, ind_airspeed) }, \
00048 { "true_airspeed", NULL, MAVLINK_TYPE_UINT16_T, 0, 56, offsetof(mavlink_hil_state_quaternion_t, true_airspeed) }, \
00049 { "xacc", NULL, MAVLINK_TYPE_INT16_T, 0, 58, offsetof(mavlink_hil_state_quaternion_t, xacc) }, \
00050 { "yacc", NULL, MAVLINK_TYPE_INT16_T, 0, 60, offsetof(mavlink_hil_state_quaternion_t, yacc) }, \
00051 { "zacc", NULL, MAVLINK_TYPE_INT16_T, 0, 62, offsetof(mavlink_hil_state_quaternion_t, zacc) }, \
00052 } \
00053 }
00054
00055
00080 static inline uint16_t mavlink_msg_hil_state_quaternion_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
00081 uint64_t time_usec, const float *attitude_quaternion, float rollspeed, float pitchspeed, float yawspeed, int32_t lat, int32_t lon, int32_t alt, int16_t vx, int16_t vy, int16_t vz, uint16_t ind_airspeed, uint16_t true_airspeed, int16_t xacc, int16_t yacc, int16_t zacc)
00082 {
00083 #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
00084 char buf[MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN];
00085 _mav_put_uint64_t(buf, 0, time_usec);
00086 _mav_put_float(buf, 24, rollspeed);
00087 _mav_put_float(buf, 28, pitchspeed);
00088 _mav_put_float(buf, 32, yawspeed);
00089 _mav_put_int32_t(buf, 36, lat);
00090 _mav_put_int32_t(buf, 40, lon);
00091 _mav_put_int32_t(buf, 44, alt);
00092 _mav_put_int16_t(buf, 48, vx);
00093 _mav_put_int16_t(buf, 50, vy);
00094 _mav_put_int16_t(buf, 52, vz);
00095 _mav_put_uint16_t(buf, 54, ind_airspeed);
00096 _mav_put_uint16_t(buf, 56, true_airspeed);
00097 _mav_put_int16_t(buf, 58, xacc);
00098 _mav_put_int16_t(buf, 60, yacc);
00099 _mav_put_int16_t(buf, 62, zacc);
00100 _mav_put_float_array(buf, 8, attitude_quaternion, 4);
00101 memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
00102 #else
00103 mavlink_hil_state_quaternion_t packet;
00104 packet.time_usec = time_usec;
00105 packet.rollspeed = rollspeed;
00106 packet.pitchspeed = pitchspeed;
00107 packet.yawspeed = yawspeed;
00108 packet.lat = lat;
00109 packet.lon = lon;
00110 packet.alt = alt;
00111 packet.vx = vx;
00112 packet.vy = vy;
00113 packet.vz = vz;
00114 packet.ind_airspeed = ind_airspeed;
00115 packet.true_airspeed = true_airspeed;
00116 packet.xacc = xacc;
00117 packet.yacc = yacc;
00118 packet.zacc = zacc;
00119 mav_array_memcpy(packet.attitude_quaternion, attitude_quaternion, sizeof(float)*4);
00120 memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
00121 #endif
00122
00123 msg->msgid = MAVLINK_MSG_ID_HIL_STATE_QUATERNION;
00124 #if MAVLINK_CRC_EXTRA
00125 return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC);
00126 #else
00127 return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
00128 #endif
00129 }
00130
00155 static inline uint16_t mavlink_msg_hil_state_quaternion_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
00156 mavlink_message_t* msg,
00157 uint64_t time_usec,const float *attitude_quaternion,float rollspeed,float pitchspeed,float yawspeed,int32_t lat,int32_t lon,int32_t alt,int16_t vx,int16_t vy,int16_t vz,uint16_t ind_airspeed,uint16_t true_airspeed,int16_t xacc,int16_t yacc,int16_t zacc)
00158 {
00159 #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
00160 char buf[MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN];
00161 _mav_put_uint64_t(buf, 0, time_usec);
00162 _mav_put_float(buf, 24, rollspeed);
00163 _mav_put_float(buf, 28, pitchspeed);
00164 _mav_put_float(buf, 32, yawspeed);
00165 _mav_put_int32_t(buf, 36, lat);
00166 _mav_put_int32_t(buf, 40, lon);
00167 _mav_put_int32_t(buf, 44, alt);
00168 _mav_put_int16_t(buf, 48, vx);
00169 _mav_put_int16_t(buf, 50, vy);
00170 _mav_put_int16_t(buf, 52, vz);
00171 _mav_put_uint16_t(buf, 54, ind_airspeed);
00172 _mav_put_uint16_t(buf, 56, true_airspeed);
00173 _mav_put_int16_t(buf, 58, xacc);
00174 _mav_put_int16_t(buf, 60, yacc);
00175 _mav_put_int16_t(buf, 62, zacc);
00176 _mav_put_float_array(buf, 8, attitude_quaternion, 4);
00177 memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
00178 #else
00179 mavlink_hil_state_quaternion_t packet;
00180 packet.time_usec = time_usec;
00181 packet.rollspeed = rollspeed;
00182 packet.pitchspeed = pitchspeed;
00183 packet.yawspeed = yawspeed;
00184 packet.lat = lat;
00185 packet.lon = lon;
00186 packet.alt = alt;
00187 packet.vx = vx;
00188 packet.vy = vy;
00189 packet.vz = vz;
00190 packet.ind_airspeed = ind_airspeed;
00191 packet.true_airspeed = true_airspeed;
00192 packet.xacc = xacc;
00193 packet.yacc = yacc;
00194 packet.zacc = zacc;
00195 mav_array_memcpy(packet.attitude_quaternion, attitude_quaternion, sizeof(float)*4);
00196 memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
00197 #endif
00198
00199 msg->msgid = MAVLINK_MSG_ID_HIL_STATE_QUATERNION;
00200 #if MAVLINK_CRC_EXTRA
00201 return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC);
00202 #else
00203 return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
00204 #endif
00205 }
00206
00215 static inline uint16_t mavlink_msg_hil_state_quaternion_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_hil_state_quaternion_t* hil_state_quaternion)
00216 {
00217 return mavlink_msg_hil_state_quaternion_pack(system_id, component_id, msg, hil_state_quaternion->time_usec, hil_state_quaternion->attitude_quaternion, hil_state_quaternion->rollspeed, hil_state_quaternion->pitchspeed, hil_state_quaternion->yawspeed, hil_state_quaternion->lat, hil_state_quaternion->lon, hil_state_quaternion->alt, hil_state_quaternion->vx, hil_state_quaternion->vy, hil_state_quaternion->vz, hil_state_quaternion->ind_airspeed, hil_state_quaternion->true_airspeed, hil_state_quaternion->xacc, hil_state_quaternion->yacc, hil_state_quaternion->zacc);
00218 }
00219
00229 static inline uint16_t mavlink_msg_hil_state_quaternion_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_hil_state_quaternion_t* hil_state_quaternion)
00230 {
00231 return mavlink_msg_hil_state_quaternion_pack_chan(system_id, component_id, chan, msg, hil_state_quaternion->time_usec, hil_state_quaternion->attitude_quaternion, hil_state_quaternion->rollspeed, hil_state_quaternion->pitchspeed, hil_state_quaternion->yawspeed, hil_state_quaternion->lat, hil_state_quaternion->lon, hil_state_quaternion->alt, hil_state_quaternion->vx, hil_state_quaternion->vy, hil_state_quaternion->vz, hil_state_quaternion->ind_airspeed, hil_state_quaternion->true_airspeed, hil_state_quaternion->xacc, hil_state_quaternion->yacc, hil_state_quaternion->zacc);
00232 }
00233
00255 #ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
00256
00257 static inline void mavlink_msg_hil_state_quaternion_send(mavlink_channel_t chan, uint64_t time_usec, const float *attitude_quaternion, float rollspeed, float pitchspeed, float yawspeed, int32_t lat, int32_t lon, int32_t alt, int16_t vx, int16_t vy, int16_t vz, uint16_t ind_airspeed, uint16_t true_airspeed, int16_t xacc, int16_t yacc, int16_t zacc)
00258 {
00259 #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
00260 char buf[MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN];
00261 _mav_put_uint64_t(buf, 0, time_usec);
00262 _mav_put_float(buf, 24, rollspeed);
00263 _mav_put_float(buf, 28, pitchspeed);
00264 _mav_put_float(buf, 32, yawspeed);
00265 _mav_put_int32_t(buf, 36, lat);
00266 _mav_put_int32_t(buf, 40, lon);
00267 _mav_put_int32_t(buf, 44, alt);
00268 _mav_put_int16_t(buf, 48, vx);
00269 _mav_put_int16_t(buf, 50, vy);
00270 _mav_put_int16_t(buf, 52, vz);
00271 _mav_put_uint16_t(buf, 54, ind_airspeed);
00272 _mav_put_uint16_t(buf, 56, true_airspeed);
00273 _mav_put_int16_t(buf, 58, xacc);
00274 _mav_put_int16_t(buf, 60, yacc);
00275 _mav_put_int16_t(buf, 62, zacc);
00276 _mav_put_float_array(buf, 8, attitude_quaternion, 4);
00277 #if MAVLINK_CRC_EXTRA
00278 _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC);
00279 #else
00280 _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
00281 #endif
00282 #else
00283 mavlink_hil_state_quaternion_t packet;
00284 packet.time_usec = time_usec;
00285 packet.rollspeed = rollspeed;
00286 packet.pitchspeed = pitchspeed;
00287 packet.yawspeed = yawspeed;
00288 packet.lat = lat;
00289 packet.lon = lon;
00290 packet.alt = alt;
00291 packet.vx = vx;
00292 packet.vy = vy;
00293 packet.vz = vz;
00294 packet.ind_airspeed = ind_airspeed;
00295 packet.true_airspeed = true_airspeed;
00296 packet.xacc = xacc;
00297 packet.yacc = yacc;
00298 packet.zacc = zacc;
00299 mav_array_memcpy(packet.attitude_quaternion, attitude_quaternion, sizeof(float)*4);
00300 #if MAVLINK_CRC_EXTRA
00301 _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, (const char *)&packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC);
00302 #else
00303 _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, (const char *)&packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
00304 #endif
00305 #endif
00306 }
00307
00308 #if MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN <= MAVLINK_MAX_PAYLOAD_LEN
00309
00310
00311
00312
00313
00314
00315
00316 static inline void mavlink_msg_hil_state_quaternion_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t time_usec, const float *attitude_quaternion, float rollspeed, float pitchspeed, float yawspeed, int32_t lat, int32_t lon, int32_t alt, int16_t vx, int16_t vy, int16_t vz, uint16_t ind_airspeed, uint16_t true_airspeed, int16_t xacc, int16_t yacc, int16_t zacc)
00317 {
00318 #if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
00319 char *buf = (char *)msgbuf;
00320 _mav_put_uint64_t(buf, 0, time_usec);
00321 _mav_put_float(buf, 24, rollspeed);
00322 _mav_put_float(buf, 28, pitchspeed);
00323 _mav_put_float(buf, 32, yawspeed);
00324 _mav_put_int32_t(buf, 36, lat);
00325 _mav_put_int32_t(buf, 40, lon);
00326 _mav_put_int32_t(buf, 44, alt);
00327 _mav_put_int16_t(buf, 48, vx);
00328 _mav_put_int16_t(buf, 50, vy);
00329 _mav_put_int16_t(buf, 52, vz);
00330 _mav_put_uint16_t(buf, 54, ind_airspeed);
00331 _mav_put_uint16_t(buf, 56, true_airspeed);
00332 _mav_put_int16_t(buf, 58, xacc);
00333 _mav_put_int16_t(buf, 60, yacc);
00334 _mav_put_int16_t(buf, 62, zacc);
00335 _mav_put_float_array(buf, 8, attitude_quaternion, 4);
00336 #if MAVLINK_CRC_EXTRA
00337 _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC);
00338 #else
00339 _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
00340 #endif
00341 #else
00342 mavlink_hil_state_quaternion_t *packet = (mavlink_hil_state_quaternion_t *)msgbuf;
00343 packet->time_usec = time_usec;
00344 packet->rollspeed = rollspeed;
00345 packet->pitchspeed = pitchspeed;
00346 packet->yawspeed = yawspeed;
00347 packet->lat = lat;
00348 packet->lon = lon;
00349 packet->alt = alt;
00350 packet->vx = vx;
00351 packet->vy = vy;
00352 packet->vz = vz;
00353 packet->ind_airspeed = ind_airspeed;
00354 packet->true_airspeed = true_airspeed;
00355 packet->xacc = xacc;
00356 packet->yacc = yacc;
00357 packet->zacc = zacc;
00358 mav_array_memcpy(packet->attitude_quaternion, attitude_quaternion, sizeof(float)*4);
00359 #if MAVLINK_CRC_EXTRA
00360 _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, (const char *)packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC);
00361 #else
00362 _mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, (const char *)packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
00363 #endif
00364 #endif
00365 }
00366 #endif
00367
00368 #endif
00369
00370
00371
00372
00378 static inline uint64_t mavlink_msg_hil_state_quaternion_get_time_usec(const mavlink_message_t* msg)
00379 {
00380 return _MAV_RETURN_uint64_t(msg, 0);
00381 }
00382
00388 static inline uint16_t mavlink_msg_hil_state_quaternion_get_attitude_quaternion(const mavlink_message_t* msg, float *attitude_quaternion)
00389 {
00390 return _MAV_RETURN_float_array(msg, attitude_quaternion, 4, 8);
00391 }
00392
00398 static inline float mavlink_msg_hil_state_quaternion_get_rollspeed(const mavlink_message_t* msg)
00399 {
00400 return _MAV_RETURN_float(msg, 24);
00401 }
00402
00408 static inline float mavlink_msg_hil_state_quaternion_get_pitchspeed(const mavlink_message_t* msg)
00409 {
00410 return _MAV_RETURN_float(msg, 28);
00411 }
00412
00418 static inline float mavlink_msg_hil_state_quaternion_get_yawspeed(const mavlink_message_t* msg)
00419 {
00420 return _MAV_RETURN_float(msg, 32);
00421 }
00422
00428 static inline int32_t mavlink_msg_hil_state_quaternion_get_lat(const mavlink_message_t* msg)
00429 {
00430 return _MAV_RETURN_int32_t(msg, 36);
00431 }
00432
00438 static inline int32_t mavlink_msg_hil_state_quaternion_get_lon(const mavlink_message_t* msg)
00439 {
00440 return _MAV_RETURN_int32_t(msg, 40);
00441 }
00442
00448 static inline int32_t mavlink_msg_hil_state_quaternion_get_alt(const mavlink_message_t* msg)
00449 {
00450 return _MAV_RETURN_int32_t(msg, 44);
00451 }
00452
00458 static inline int16_t mavlink_msg_hil_state_quaternion_get_vx(const mavlink_message_t* msg)
00459 {
00460 return _MAV_RETURN_int16_t(msg, 48);
00461 }
00462
00468 static inline int16_t mavlink_msg_hil_state_quaternion_get_vy(const mavlink_message_t* msg)
00469 {
00470 return _MAV_RETURN_int16_t(msg, 50);
00471 }
00472
00478 static inline int16_t mavlink_msg_hil_state_quaternion_get_vz(const mavlink_message_t* msg)
00479 {
00480 return _MAV_RETURN_int16_t(msg, 52);
00481 }
00482
00488 static inline uint16_t mavlink_msg_hil_state_quaternion_get_ind_airspeed(const mavlink_message_t* msg)
00489 {
00490 return _MAV_RETURN_uint16_t(msg, 54);
00491 }
00492
00498 static inline uint16_t mavlink_msg_hil_state_quaternion_get_true_airspeed(const mavlink_message_t* msg)
00499 {
00500 return _MAV_RETURN_uint16_t(msg, 56);
00501 }
00502
00508 static inline int16_t mavlink_msg_hil_state_quaternion_get_xacc(const mavlink_message_t* msg)
00509 {
00510 return _MAV_RETURN_int16_t(msg, 58);
00511 }
00512
00518 static inline int16_t mavlink_msg_hil_state_quaternion_get_yacc(const mavlink_message_t* msg)
00519 {
00520 return _MAV_RETURN_int16_t(msg, 60);
00521 }
00522
00528 static inline int16_t mavlink_msg_hil_state_quaternion_get_zacc(const mavlink_message_t* msg)
00529 {
00530 return _MAV_RETURN_int16_t(msg, 62);
00531 }
00532
00539 static inline void mavlink_msg_hil_state_quaternion_decode(const mavlink_message_t* msg, mavlink_hil_state_quaternion_t* hil_state_quaternion)
00540 {
00541 #if MAVLINK_NEED_BYTE_SWAP
00542 hil_state_quaternion->time_usec = mavlink_msg_hil_state_quaternion_get_time_usec(msg);
00543 mavlink_msg_hil_state_quaternion_get_attitude_quaternion(msg, hil_state_quaternion->attitude_quaternion);
00544 hil_state_quaternion->rollspeed = mavlink_msg_hil_state_quaternion_get_rollspeed(msg);
00545 hil_state_quaternion->pitchspeed = mavlink_msg_hil_state_quaternion_get_pitchspeed(msg);
00546 hil_state_quaternion->yawspeed = mavlink_msg_hil_state_quaternion_get_yawspeed(msg);
00547 hil_state_quaternion->lat = mavlink_msg_hil_state_quaternion_get_lat(msg);
00548 hil_state_quaternion->lon = mavlink_msg_hil_state_quaternion_get_lon(msg);
00549 hil_state_quaternion->alt = mavlink_msg_hil_state_quaternion_get_alt(msg);
00550 hil_state_quaternion->vx = mavlink_msg_hil_state_quaternion_get_vx(msg);
00551 hil_state_quaternion->vy = mavlink_msg_hil_state_quaternion_get_vy(msg);
00552 hil_state_quaternion->vz = mavlink_msg_hil_state_quaternion_get_vz(msg);
00553 hil_state_quaternion->ind_airspeed = mavlink_msg_hil_state_quaternion_get_ind_airspeed(msg);
00554 hil_state_quaternion->true_airspeed = mavlink_msg_hil_state_quaternion_get_true_airspeed(msg);
00555 hil_state_quaternion->xacc = mavlink_msg_hil_state_quaternion_get_xacc(msg);
00556 hil_state_quaternion->yacc = mavlink_msg_hil_state_quaternion_get_yacc(msg);
00557 hil_state_quaternion->zacc = mavlink_msg_hil_state_quaternion_get_zacc(msg);
00558 #else
00559 memcpy(hil_state_quaternion, _MAV_PAYLOAD(msg), MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
00560 #endif
00561 }