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autogenerated headers for rev https://github.com/mavlink/mavlink/tree/6484834917efebc03f7f0326474fc235c2f5e000

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This commit is contained in:
PX4BuildBot
2016-10-10 10:40:57 +00:00
parent 78b639c348
commit f038d1f0b5
283 changed files with 29211 additions and 29211 deletions
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common/mavlink_msg_hil_state_quaternion.h
+183 -183
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@@ -35,10 +35,10 @@ typedef struct __mavlink_hil_state_quaternion_t {
#if MAVLINK_COMMAND_24BIT
#define MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION { \
115, \
"HIL_STATE_QUATERNION", \
16, \
{ { "time_usec", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_hil_state_quaternion_t, time_usec) }, \
115, \
"HIL_STATE_QUATERNION", \
16, \
{ { "time_usec", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_hil_state_quaternion_t, time_usec) }, \
{ "attitude_quaternion", NULL, MAVLINK_TYPE_FLOAT, 4, 8, offsetof(mavlink_hil_state_quaternion_t, attitude_quaternion) }, \
{ "rollspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_hil_state_quaternion_t, rollspeed) }, \
{ "pitchspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_hil_state_quaternion_t, pitchspeed) }, \
@@ -58,9 +58,9 @@ typedef struct __mavlink_hil_state_quaternion_t {
}
#else
#define MAVLINK_MESSAGE_INFO_HIL_STATE_QUATERNION { \
"HIL_STATE_QUATERNION", \
16, \
{ { "time_usec", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_hil_state_quaternion_t, time_usec) }, \
"HIL_STATE_QUATERNION", \
16, \
{ { "time_usec", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_hil_state_quaternion_t, time_usec) }, \
{ "attitude_quaternion", NULL, MAVLINK_TYPE_FLOAT, 4, 8, offsetof(mavlink_hil_state_quaternion_t, attitude_quaternion) }, \
{ "rollspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_hil_state_quaternion_t, rollspeed) }, \
{ "pitchspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_hil_state_quaternion_t, pitchspeed) }, \
@@ -105,49 +105,49 @@ typedef struct __mavlink_hil_state_quaternion_t {
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_hil_state_quaternion_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
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)
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)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN];
_mav_put_uint64_t(buf, 0, time_usec);
_mav_put_float(buf, 24, rollspeed);
_mav_put_float(buf, 28, pitchspeed);
_mav_put_float(buf, 32, yawspeed);
_mav_put_int32_t(buf, 36, lat);
_mav_put_int32_t(buf, 40, lon);
_mav_put_int32_t(buf, 44, alt);
_mav_put_int16_t(buf, 48, vx);
_mav_put_int16_t(buf, 50, vy);
_mav_put_int16_t(buf, 52, vz);
_mav_put_uint16_t(buf, 54, ind_airspeed);
_mav_put_uint16_t(buf, 56, true_airspeed);
_mav_put_int16_t(buf, 58, xacc);
_mav_put_int16_t(buf, 60, yacc);
_mav_put_int16_t(buf, 62, zacc);
_mav_put_float_array(buf, 8, attitude_quaternion, 4);
char buf[MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN];
_mav_put_uint64_t(buf, 0, time_usec);
_mav_put_float(buf, 24, rollspeed);
_mav_put_float(buf, 28, pitchspeed);
_mav_put_float(buf, 32, yawspeed);
_mav_put_int32_t(buf, 36, lat);
_mav_put_int32_t(buf, 40, lon);
_mav_put_int32_t(buf, 44, alt);
_mav_put_int16_t(buf, 48, vx);
_mav_put_int16_t(buf, 50, vy);
_mav_put_int16_t(buf, 52, vz);
_mav_put_uint16_t(buf, 54, ind_airspeed);
_mav_put_uint16_t(buf, 56, true_airspeed);
_mav_put_int16_t(buf, 58, xacc);
_mav_put_int16_t(buf, 60, yacc);
_mav_put_int16_t(buf, 62, zacc);
_mav_put_float_array(buf, 8, attitude_quaternion, 4);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
#else
mavlink_hil_state_quaternion_t packet;
packet.time_usec = time_usec;
packet.rollspeed = rollspeed;
packet.pitchspeed = pitchspeed;
packet.yawspeed = yawspeed;
packet.lat = lat;
packet.lon = lon;
packet.alt = alt;
packet.vx = vx;
packet.vy = vy;
packet.vz = vz;
packet.ind_airspeed = ind_airspeed;
packet.true_airspeed = true_airspeed;
packet.xacc = xacc;
packet.yacc = yacc;
packet.zacc = zacc;
mav_array_memcpy(packet.attitude_quaternion, attitude_quaternion, sizeof(float)*4);
mavlink_hil_state_quaternion_t packet;
packet.time_usec = time_usec;
packet.rollspeed = rollspeed;
packet.pitchspeed = pitchspeed;
packet.yawspeed = yawspeed;
packet.lat = lat;
packet.lon = lon;
packet.alt = alt;
packet.vx = vx;
packet.vy = vy;
packet.vz = vz;
packet.ind_airspeed = ind_airspeed;
packet.true_airspeed = true_airspeed;
packet.xacc = xacc;
packet.yacc = yacc;
packet.zacc = zacc;
mav_array_memcpy(packet.attitude_quaternion, attitude_quaternion, sizeof(float)*4);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_HIL_STATE_QUATERNION;
msg->msgid = MAVLINK_MSG_ID_HIL_STATE_QUATERNION;
return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_MIN_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC);
}
@@ -176,50 +176,50 @@ static inline uint16_t mavlink_msg_hil_state_quaternion_pack(uint8_t system_id,
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_hil_state_quaternion_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
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)
mavlink_message_t* msg,
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)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN];
_mav_put_uint64_t(buf, 0, time_usec);
_mav_put_float(buf, 24, rollspeed);
_mav_put_float(buf, 28, pitchspeed);
_mav_put_float(buf, 32, yawspeed);
_mav_put_int32_t(buf, 36, lat);
_mav_put_int32_t(buf, 40, lon);
_mav_put_int32_t(buf, 44, alt);
_mav_put_int16_t(buf, 48, vx);
_mav_put_int16_t(buf, 50, vy);
_mav_put_int16_t(buf, 52, vz);
_mav_put_uint16_t(buf, 54, ind_airspeed);
_mav_put_uint16_t(buf, 56, true_airspeed);
_mav_put_int16_t(buf, 58, xacc);
_mav_put_int16_t(buf, 60, yacc);
_mav_put_int16_t(buf, 62, zacc);
_mav_put_float_array(buf, 8, attitude_quaternion, 4);
char buf[MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN];
_mav_put_uint64_t(buf, 0, time_usec);
_mav_put_float(buf, 24, rollspeed);
_mav_put_float(buf, 28, pitchspeed);
_mav_put_float(buf, 32, yawspeed);
_mav_put_int32_t(buf, 36, lat);
_mav_put_int32_t(buf, 40, lon);
_mav_put_int32_t(buf, 44, alt);
_mav_put_int16_t(buf, 48, vx);
_mav_put_int16_t(buf, 50, vy);
_mav_put_int16_t(buf, 52, vz);
_mav_put_uint16_t(buf, 54, ind_airspeed);
_mav_put_uint16_t(buf, 56, true_airspeed);
_mav_put_int16_t(buf, 58, xacc);
_mav_put_int16_t(buf, 60, yacc);
_mav_put_int16_t(buf, 62, zacc);
_mav_put_float_array(buf, 8, attitude_quaternion, 4);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
#else
mavlink_hil_state_quaternion_t packet;
packet.time_usec = time_usec;
packet.rollspeed = rollspeed;
packet.pitchspeed = pitchspeed;
packet.yawspeed = yawspeed;
packet.lat = lat;
packet.lon = lon;
packet.alt = alt;
packet.vx = vx;
packet.vy = vy;
packet.vz = vz;
packet.ind_airspeed = ind_airspeed;
packet.true_airspeed = true_airspeed;
packet.xacc = xacc;
packet.yacc = yacc;
packet.zacc = zacc;
mav_array_memcpy(packet.attitude_quaternion, attitude_quaternion, sizeof(float)*4);
mavlink_hil_state_quaternion_t packet;
packet.time_usec = time_usec;
packet.rollspeed = rollspeed;
packet.pitchspeed = pitchspeed;
packet.yawspeed = yawspeed;
packet.lat = lat;
packet.lon = lon;
packet.alt = alt;
packet.vx = vx;
packet.vy = vy;
packet.vz = vz;
packet.ind_airspeed = ind_airspeed;
packet.true_airspeed = true_airspeed;
packet.xacc = xacc;
packet.yacc = yacc;
packet.zacc = zacc;
mav_array_memcpy(packet.attitude_quaternion, attitude_quaternion, sizeof(float)*4);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_HIL_STATE_QUATERNION;
msg->msgid = MAVLINK_MSG_ID_HIL_STATE_QUATERNION;
return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_MIN_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC);
}
@@ -233,7 +233,7 @@ static inline uint16_t mavlink_msg_hil_state_quaternion_pack_chan(uint8_t system
*/
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)
{
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);
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);
}
/**
@@ -247,7 +247,7 @@ static inline uint16_t mavlink_msg_hil_state_quaternion_encode(uint8_t system_id
*/
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)
{
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);
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);
}
/**
@@ -276,42 +276,42 @@ static inline uint16_t mavlink_msg_hil_state_quaternion_encode_chan(uint8_t syst
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)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN];
_mav_put_uint64_t(buf, 0, time_usec);
_mav_put_float(buf, 24, rollspeed);
_mav_put_float(buf, 28, pitchspeed);
_mav_put_float(buf, 32, yawspeed);
_mav_put_int32_t(buf, 36, lat);
_mav_put_int32_t(buf, 40, lon);
_mav_put_int32_t(buf, 44, alt);
_mav_put_int16_t(buf, 48, vx);
_mav_put_int16_t(buf, 50, vy);
_mav_put_int16_t(buf, 52, vz);
_mav_put_uint16_t(buf, 54, ind_airspeed);
_mav_put_uint16_t(buf, 56, true_airspeed);
_mav_put_int16_t(buf, 58, xacc);
_mav_put_int16_t(buf, 60, yacc);
_mav_put_int16_t(buf, 62, zacc);
_mav_put_float_array(buf, 8, attitude_quaternion, 4);
char buf[MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN];
_mav_put_uint64_t(buf, 0, time_usec);
_mav_put_float(buf, 24, rollspeed);
_mav_put_float(buf, 28, pitchspeed);
_mav_put_float(buf, 32, yawspeed);
_mav_put_int32_t(buf, 36, lat);
_mav_put_int32_t(buf, 40, lon);
_mav_put_int32_t(buf, 44, alt);
_mav_put_int16_t(buf, 48, vx);
_mav_put_int16_t(buf, 50, vy);
_mav_put_int16_t(buf, 52, vz);
_mav_put_uint16_t(buf, 54, ind_airspeed);
_mav_put_uint16_t(buf, 56, true_airspeed);
_mav_put_int16_t(buf, 58, xacc);
_mav_put_int16_t(buf, 60, yacc);
_mav_put_int16_t(buf, 62, zacc);
_mav_put_float_array(buf, 8, attitude_quaternion, 4);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_MIN_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC);
#else
mavlink_hil_state_quaternion_t packet;
packet.time_usec = time_usec;
packet.rollspeed = rollspeed;
packet.pitchspeed = pitchspeed;
packet.yawspeed = yawspeed;
packet.lat = lat;
packet.lon = lon;
packet.alt = alt;
packet.vx = vx;
packet.vy = vy;
packet.vz = vz;
packet.ind_airspeed = ind_airspeed;
packet.true_airspeed = true_airspeed;
packet.xacc = xacc;
packet.yacc = yacc;
packet.zacc = zacc;
mav_array_memcpy(packet.attitude_quaternion, attitude_quaternion, sizeof(float)*4);
mavlink_hil_state_quaternion_t packet;
packet.time_usec = time_usec;
packet.rollspeed = rollspeed;
packet.pitchspeed = pitchspeed;
packet.yawspeed = yawspeed;
packet.lat = lat;
packet.lon = lon;
packet.alt = alt;
packet.vx = vx;
packet.vy = vy;
packet.vz = vz;
packet.ind_airspeed = ind_airspeed;
packet.true_airspeed = true_airspeed;
packet.xacc = xacc;
packet.yacc = yacc;
packet.zacc = zacc;
mav_array_memcpy(packet.attitude_quaternion, attitude_quaternion, sizeof(float)*4);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, (const char *)&packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_MIN_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC);
#endif
}
@@ -341,42 +341,42 @@ static inline void mavlink_msg_hil_state_quaternion_send_struct(mavlink_channel_
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)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
_mav_put_uint64_t(buf, 0, time_usec);
_mav_put_float(buf, 24, rollspeed);
_mav_put_float(buf, 28, pitchspeed);
_mav_put_float(buf, 32, yawspeed);
_mav_put_int32_t(buf, 36, lat);
_mav_put_int32_t(buf, 40, lon);
_mav_put_int32_t(buf, 44, alt);
_mav_put_int16_t(buf, 48, vx);
_mav_put_int16_t(buf, 50, vy);
_mav_put_int16_t(buf, 52, vz);
_mav_put_uint16_t(buf, 54, ind_airspeed);
_mav_put_uint16_t(buf, 56, true_airspeed);
_mav_put_int16_t(buf, 58, xacc);
_mav_put_int16_t(buf, 60, yacc);
_mav_put_int16_t(buf, 62, zacc);
_mav_put_float_array(buf, 8, attitude_quaternion, 4);
char *buf = (char *)msgbuf;
_mav_put_uint64_t(buf, 0, time_usec);
_mav_put_float(buf, 24, rollspeed);
_mav_put_float(buf, 28, pitchspeed);
_mav_put_float(buf, 32, yawspeed);
_mav_put_int32_t(buf, 36, lat);
_mav_put_int32_t(buf, 40, lon);
_mav_put_int32_t(buf, 44, alt);
_mav_put_int16_t(buf, 48, vx);
_mav_put_int16_t(buf, 50, vy);
_mav_put_int16_t(buf, 52, vz);
_mav_put_uint16_t(buf, 54, ind_airspeed);
_mav_put_uint16_t(buf, 56, true_airspeed);
_mav_put_int16_t(buf, 58, xacc);
_mav_put_int16_t(buf, 60, yacc);
_mav_put_int16_t(buf, 62, zacc);
_mav_put_float_array(buf, 8, attitude_quaternion, 4);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_MIN_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC);
#else
mavlink_hil_state_quaternion_t *packet = (mavlink_hil_state_quaternion_t *)msgbuf;
packet->time_usec = time_usec;
packet->rollspeed = rollspeed;
packet->pitchspeed = pitchspeed;
packet->yawspeed = yawspeed;
packet->lat = lat;
packet->lon = lon;
packet->alt = alt;
packet->vx = vx;
packet->vy = vy;
packet->vz = vz;
packet->ind_airspeed = ind_airspeed;
packet->true_airspeed = true_airspeed;
packet->xacc = xacc;
packet->yacc = yacc;
packet->zacc = zacc;
mav_array_memcpy(packet->attitude_quaternion, attitude_quaternion, sizeof(float)*4);
mavlink_hil_state_quaternion_t *packet = (mavlink_hil_state_quaternion_t *)msgbuf;
packet->time_usec = time_usec;
packet->rollspeed = rollspeed;
packet->pitchspeed = pitchspeed;
packet->yawspeed = yawspeed;
packet->lat = lat;
packet->lon = lon;
packet->alt = alt;
packet->vx = vx;
packet->vy = vy;
packet->vz = vz;
packet->ind_airspeed = ind_airspeed;
packet->true_airspeed = true_airspeed;
packet->xacc = xacc;
packet->yacc = yacc;
packet->zacc = zacc;
mav_array_memcpy(packet->attitude_quaternion, attitude_quaternion, sizeof(float)*4);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_HIL_STATE_QUATERNION, (const char *)packet, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_MIN_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC);
#endif
}
@@ -394,7 +394,7 @@ static inline void mavlink_msg_hil_state_quaternion_send_buf(mavlink_message_t *
*/
static inline uint64_t mavlink_msg_hil_state_quaternion_get_time_usec(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint64_t(msg, 0);
return _MAV_RETURN_uint64_t(msg, 0);
}
/**
@@ -404,7 +404,7 @@ static inline uint64_t mavlink_msg_hil_state_quaternion_get_time_usec(const mavl
*/
static inline uint16_t mavlink_msg_hil_state_quaternion_get_attitude_quaternion(const mavlink_message_t* msg, float *attitude_quaternion)
{
return _MAV_RETURN_float_array(msg, attitude_quaternion, 4, 8);
return _MAV_RETURN_float_array(msg, attitude_quaternion, 4, 8);
}
/**
@@ -414,7 +414,7 @@ static inline uint16_t mavlink_msg_hil_state_quaternion_get_attitude_quaternion(
*/
static inline float mavlink_msg_hil_state_quaternion_get_rollspeed(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 24);
return _MAV_RETURN_float(msg, 24);
}
/**
@@ -424,7 +424,7 @@ static inline float mavlink_msg_hil_state_quaternion_get_rollspeed(const mavlink
*/
static inline float mavlink_msg_hil_state_quaternion_get_pitchspeed(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 28);
return _MAV_RETURN_float(msg, 28);
}
/**
@@ -434,7 +434,7 @@ static inline float mavlink_msg_hil_state_quaternion_get_pitchspeed(const mavlin
*/
static inline float mavlink_msg_hil_state_quaternion_get_yawspeed(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 32);
return _MAV_RETURN_float(msg, 32);
}
/**
@@ -444,7 +444,7 @@ static inline float mavlink_msg_hil_state_quaternion_get_yawspeed(const mavlink_
*/
static inline int32_t mavlink_msg_hil_state_quaternion_get_lat(const mavlink_message_t* msg)
{
return _MAV_RETURN_int32_t(msg, 36);
return _MAV_RETURN_int32_t(msg, 36);
}
/**
@@ -454,7 +454,7 @@ static inline int32_t mavlink_msg_hil_state_quaternion_get_lat(const mavlink_mes
*/
static inline int32_t mavlink_msg_hil_state_quaternion_get_lon(const mavlink_message_t* msg)
{
return _MAV_RETURN_int32_t(msg, 40);
return _MAV_RETURN_int32_t(msg, 40);
}
/**
@@ -464,7 +464,7 @@ static inline int32_t mavlink_msg_hil_state_quaternion_get_lon(const mavlink_mes
*/
static inline int32_t mavlink_msg_hil_state_quaternion_get_alt(const mavlink_message_t* msg)
{
return _MAV_RETURN_int32_t(msg, 44);
return _MAV_RETURN_int32_t(msg, 44);
}
/**
@@ -474,7 +474,7 @@ static inline int32_t mavlink_msg_hil_state_quaternion_get_alt(const mavlink_mes
*/
static inline int16_t mavlink_msg_hil_state_quaternion_get_vx(const mavlink_message_t* msg)
{
return _MAV_RETURN_int16_t(msg, 48);
return _MAV_RETURN_int16_t(msg, 48);
}
/**
@@ -484,7 +484,7 @@ static inline int16_t mavlink_msg_hil_state_quaternion_get_vx(const mavlink_mess
*/
static inline int16_t mavlink_msg_hil_state_quaternion_get_vy(const mavlink_message_t* msg)
{
return _MAV_RETURN_int16_t(msg, 50);
return _MAV_RETURN_int16_t(msg, 50);
}
/**
@@ -494,7 +494,7 @@ static inline int16_t mavlink_msg_hil_state_quaternion_get_vy(const mavlink_mess
*/
static inline int16_t mavlink_msg_hil_state_quaternion_get_vz(const mavlink_message_t* msg)
{
return _MAV_RETURN_int16_t(msg, 52);
return _MAV_RETURN_int16_t(msg, 52);
}
/**
@@ -504,7 +504,7 @@ static inline int16_t mavlink_msg_hil_state_quaternion_get_vz(const mavlink_mess
*/
static inline uint16_t mavlink_msg_hil_state_quaternion_get_ind_airspeed(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 54);
return _MAV_RETURN_uint16_t(msg, 54);
}
/**
@@ -514,7 +514,7 @@ static inline uint16_t mavlink_msg_hil_state_quaternion_get_ind_airspeed(const m
*/
static inline uint16_t mavlink_msg_hil_state_quaternion_get_true_airspeed(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 56);
return _MAV_RETURN_uint16_t(msg, 56);
}
/**
@@ -524,7 +524,7 @@ static inline uint16_t mavlink_msg_hil_state_quaternion_get_true_airspeed(const
*/
static inline int16_t mavlink_msg_hil_state_quaternion_get_xacc(const mavlink_message_t* msg)
{
return _MAV_RETURN_int16_t(msg, 58);
return _MAV_RETURN_int16_t(msg, 58);
}
/**
@@ -534,7 +534,7 @@ static inline int16_t mavlink_msg_hil_state_quaternion_get_xacc(const mavlink_me
*/
static inline int16_t mavlink_msg_hil_state_quaternion_get_yacc(const mavlink_message_t* msg)
{
return _MAV_RETURN_int16_t(msg, 60);
return _MAV_RETURN_int16_t(msg, 60);
}
/**
@@ -544,7 +544,7 @@ static inline int16_t mavlink_msg_hil_state_quaternion_get_yacc(const mavlink_me
*/
static inline int16_t mavlink_msg_hil_state_quaternion_get_zacc(const mavlink_message_t* msg)
{
return _MAV_RETURN_int16_t(msg, 62);
return _MAV_RETURN_int16_t(msg, 62);
}
/**
@@ -556,25 +556,25 @@ static inline int16_t mavlink_msg_hil_state_quaternion_get_zacc(const mavlink_me
static inline void mavlink_msg_hil_state_quaternion_decode(const mavlink_message_t* msg, mavlink_hil_state_quaternion_t* hil_state_quaternion)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
hil_state_quaternion->time_usec = mavlink_msg_hil_state_quaternion_get_time_usec(msg);
mavlink_msg_hil_state_quaternion_get_attitude_quaternion(msg, hil_state_quaternion->attitude_quaternion);
hil_state_quaternion->rollspeed = mavlink_msg_hil_state_quaternion_get_rollspeed(msg);
hil_state_quaternion->pitchspeed = mavlink_msg_hil_state_quaternion_get_pitchspeed(msg);
hil_state_quaternion->yawspeed = mavlink_msg_hil_state_quaternion_get_yawspeed(msg);
hil_state_quaternion->lat = mavlink_msg_hil_state_quaternion_get_lat(msg);
hil_state_quaternion->lon = mavlink_msg_hil_state_quaternion_get_lon(msg);
hil_state_quaternion->alt = mavlink_msg_hil_state_quaternion_get_alt(msg);
hil_state_quaternion->vx = mavlink_msg_hil_state_quaternion_get_vx(msg);
hil_state_quaternion->vy = mavlink_msg_hil_state_quaternion_get_vy(msg);
hil_state_quaternion->vz = mavlink_msg_hil_state_quaternion_get_vz(msg);
hil_state_quaternion->ind_airspeed = mavlink_msg_hil_state_quaternion_get_ind_airspeed(msg);
hil_state_quaternion->true_airspeed = mavlink_msg_hil_state_quaternion_get_true_airspeed(msg);
hil_state_quaternion->xacc = mavlink_msg_hil_state_quaternion_get_xacc(msg);
hil_state_quaternion->yacc = mavlink_msg_hil_state_quaternion_get_yacc(msg);
hil_state_quaternion->zacc = mavlink_msg_hil_state_quaternion_get_zacc(msg);
hil_state_quaternion->time_usec = mavlink_msg_hil_state_quaternion_get_time_usec(msg);
mavlink_msg_hil_state_quaternion_get_attitude_quaternion(msg, hil_state_quaternion->attitude_quaternion);
hil_state_quaternion->rollspeed = mavlink_msg_hil_state_quaternion_get_rollspeed(msg);
hil_state_quaternion->pitchspeed = mavlink_msg_hil_state_quaternion_get_pitchspeed(msg);
hil_state_quaternion->yawspeed = mavlink_msg_hil_state_quaternion_get_yawspeed(msg);
hil_state_quaternion->lat = mavlink_msg_hil_state_quaternion_get_lat(msg);
hil_state_quaternion->lon = mavlink_msg_hil_state_quaternion_get_lon(msg);
hil_state_quaternion->alt = mavlink_msg_hil_state_quaternion_get_alt(msg);
hil_state_quaternion->vx = mavlink_msg_hil_state_quaternion_get_vx(msg);
hil_state_quaternion->vy = mavlink_msg_hil_state_quaternion_get_vy(msg);
hil_state_quaternion->vz = mavlink_msg_hil_state_quaternion_get_vz(msg);
hil_state_quaternion->ind_airspeed = mavlink_msg_hil_state_quaternion_get_ind_airspeed(msg);
hil_state_quaternion->true_airspeed = mavlink_msg_hil_state_quaternion_get_true_airspeed(msg);
hil_state_quaternion->xacc = mavlink_msg_hil_state_quaternion_get_xacc(msg);
hil_state_quaternion->yacc = mavlink_msg_hil_state_quaternion_get_yacc(msg);
hil_state_quaternion->zacc = mavlink_msg_hil_state_quaternion_get_zacc(msg);
#else
uint8_t len = msg->len < MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN? msg->len : MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN;
memset(hil_state_quaternion, 0, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
memcpy(hil_state_quaternion, _MAV_PAYLOAD(msg), len);
memcpy(hil_state_quaternion, _MAV_PAYLOAD(msg), len);
#endif
}