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✨feat: 更好兼容matlab

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uin64->uint32
payload64->payload
This commit is contained in:
matt
2020-09-20 10:12:24 +08:00
parent 1465895353
commit e79d1f21fb
289 changed files with 6428 additions and 15915 deletions
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common/mavlink_msg_hil_state_quaternion.h
+130 -130
View File
@@ -3,9 +3,9 @@
#define MAVLINK_MSG_ID_HIL_STATE_QUATERNION 115
MAVPACKED(
typedef struct __mavlink_hil_state_quaternion_t {
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 the number.*/
uint32_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 the number.*/
float attitude_quaternion[4]; /*< Vehicle attitude expressed as normalized quaternion in w, x, y, z order (with 1 0 0 0 being the null-rotation)*/
float rollspeed; /*< [rad/s] Body frame roll / phi angular speed*/
float pitchspeed; /*< [rad/s] Body frame pitch / theta angular speed*/
@@ -21,15 +21,15 @@ typedef struct __mavlink_hil_state_quaternion_t {
int16_t xacc; /*< [mG] X acceleration*/
int16_t yacc; /*< [mG] Y acceleration*/
int16_t zacc; /*< [mG] Z acceleration*/
}) mavlink_hil_state_quaternion_t;
} mavlink_hil_state_quaternion_t;
#define MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN 64
#define MAVLINK_MSG_ID_HIL_STATE_QUATERNION_MIN_LEN 64
#define MAVLINK_MSG_ID_115_LEN 64
#define MAVLINK_MSG_ID_115_MIN_LEN 64
#define MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN 60
#define MAVLINK_MSG_ID_HIL_STATE_QUATERNION_MIN_LEN 60
#define MAVLINK_MSG_ID_115_LEN 60
#define MAVLINK_MSG_ID_115_MIN_LEN 60
#define MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC 4
#define MAVLINK_MSG_ID_115_CRC 4
#define MAVLINK_MSG_ID_HIL_STATE_QUATERNION_CRC 188
#define MAVLINK_MSG_ID_115_CRC 188
#define MAVLINK_MSG_HIL_STATE_QUATERNION_FIELD_ATTITUDE_QUATERNION_LEN 4
@@ -38,44 +38,44 @@ typedef struct __mavlink_hil_state_quaternion_t {
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) }, \
{ "yawspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_hil_state_quaternion_t, yawspeed) }, \
{ "lat", NULL, MAVLINK_TYPE_INT32_T, 0, 36, offsetof(mavlink_hil_state_quaternion_t, lat) }, \
{ "lon", NULL, MAVLINK_TYPE_INT32_T, 0, 40, offsetof(mavlink_hil_state_quaternion_t, lon) }, \
{ "alt", NULL, MAVLINK_TYPE_INT32_T, 0, 44, offsetof(mavlink_hil_state_quaternion_t, alt) }, \
{ "vx", NULL, MAVLINK_TYPE_INT16_T, 0, 48, offsetof(mavlink_hil_state_quaternion_t, vx) }, \
{ "vy", NULL, MAVLINK_TYPE_INT16_T, 0, 50, offsetof(mavlink_hil_state_quaternion_t, vy) }, \
{ "vz", NULL, MAVLINK_TYPE_INT16_T, 0, 52, offsetof(mavlink_hil_state_quaternion_t, vz) }, \
{ "ind_airspeed", NULL, MAVLINK_TYPE_UINT16_T, 0, 54, offsetof(mavlink_hil_state_quaternion_t, ind_airspeed) }, \
{ "true_airspeed", NULL, MAVLINK_TYPE_UINT16_T, 0, 56, offsetof(mavlink_hil_state_quaternion_t, true_airspeed) }, \
{ "xacc", NULL, MAVLINK_TYPE_INT16_T, 0, 58, offsetof(mavlink_hil_state_quaternion_t, xacc) }, \
{ "yacc", NULL, MAVLINK_TYPE_INT16_T, 0, 60, offsetof(mavlink_hil_state_quaternion_t, yacc) }, \
{ "zacc", NULL, MAVLINK_TYPE_INT16_T, 0, 62, offsetof(mavlink_hil_state_quaternion_t, zacc) }, \
{ { "time_usec", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_hil_state_quaternion_t, time_usec) }, \
{ "attitude_quaternion", NULL, MAVLINK_TYPE_FLOAT, 4, 4, offsetof(mavlink_hil_state_quaternion_t, attitude_quaternion) }, \
{ "rollspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_hil_state_quaternion_t, rollspeed) }, \
{ "pitchspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_hil_state_quaternion_t, pitchspeed) }, \
{ "yawspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_hil_state_quaternion_t, yawspeed) }, \
{ "lat", NULL, MAVLINK_TYPE_INT32_T, 0, 32, offsetof(mavlink_hil_state_quaternion_t, lat) }, \
{ "lon", NULL, MAVLINK_TYPE_INT32_T, 0, 36, offsetof(mavlink_hil_state_quaternion_t, lon) }, \
{ "alt", NULL, MAVLINK_TYPE_INT32_T, 0, 40, offsetof(mavlink_hil_state_quaternion_t, alt) }, \
{ "vx", NULL, MAVLINK_TYPE_INT16_T, 0, 44, offsetof(mavlink_hil_state_quaternion_t, vx) }, \
{ "vy", NULL, MAVLINK_TYPE_INT16_T, 0, 46, offsetof(mavlink_hil_state_quaternion_t, vy) }, \
{ "vz", NULL, MAVLINK_TYPE_INT16_T, 0, 48, offsetof(mavlink_hil_state_quaternion_t, vz) }, \
{ "ind_airspeed", NULL, MAVLINK_TYPE_UINT16_T, 0, 50, offsetof(mavlink_hil_state_quaternion_t, ind_airspeed) }, \
{ "true_airspeed", NULL, MAVLINK_TYPE_UINT16_T, 0, 52, offsetof(mavlink_hil_state_quaternion_t, true_airspeed) }, \
{ "xacc", NULL, MAVLINK_TYPE_INT16_T, 0, 54, offsetof(mavlink_hil_state_quaternion_t, xacc) }, \
{ "yacc", NULL, MAVLINK_TYPE_INT16_T, 0, 56, offsetof(mavlink_hil_state_quaternion_t, yacc) }, \
{ "zacc", NULL, MAVLINK_TYPE_INT16_T, 0, 58, offsetof(mavlink_hil_state_quaternion_t, zacc) }, \
} \
}
#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) }, \
{ "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) }, \
{ "yawspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_hil_state_quaternion_t, yawspeed) }, \
{ "lat", NULL, MAVLINK_TYPE_INT32_T, 0, 36, offsetof(mavlink_hil_state_quaternion_t, lat) }, \
{ "lon", NULL, MAVLINK_TYPE_INT32_T, 0, 40, offsetof(mavlink_hil_state_quaternion_t, lon) }, \
{ "alt", NULL, MAVLINK_TYPE_INT32_T, 0, 44, offsetof(mavlink_hil_state_quaternion_t, alt) }, \
{ "vx", NULL, MAVLINK_TYPE_INT16_T, 0, 48, offsetof(mavlink_hil_state_quaternion_t, vx) }, \
{ "vy", NULL, MAVLINK_TYPE_INT16_T, 0, 50, offsetof(mavlink_hil_state_quaternion_t, vy) }, \
{ "vz", NULL, MAVLINK_TYPE_INT16_T, 0, 52, offsetof(mavlink_hil_state_quaternion_t, vz) }, \
{ "ind_airspeed", NULL, MAVLINK_TYPE_UINT16_T, 0, 54, offsetof(mavlink_hil_state_quaternion_t, ind_airspeed) }, \
{ "true_airspeed", NULL, MAVLINK_TYPE_UINT16_T, 0, 56, offsetof(mavlink_hil_state_quaternion_t, true_airspeed) }, \
{ "xacc", NULL, MAVLINK_TYPE_INT16_T, 0, 58, offsetof(mavlink_hil_state_quaternion_t, xacc) }, \
{ "yacc", NULL, MAVLINK_TYPE_INT16_T, 0, 60, offsetof(mavlink_hil_state_quaternion_t, yacc) }, \
{ "zacc", NULL, MAVLINK_TYPE_INT16_T, 0, 62, offsetof(mavlink_hil_state_quaternion_t, zacc) }, \
{ { "time_usec", NULL, MAVLINK_TYPE_UINT32_T, 0, 0, offsetof(mavlink_hil_state_quaternion_t, time_usec) }, \
{ "attitude_quaternion", NULL, MAVLINK_TYPE_FLOAT, 4, 4, offsetof(mavlink_hil_state_quaternion_t, attitude_quaternion) }, \
{ "rollspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_hil_state_quaternion_t, rollspeed) }, \
{ "pitchspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_hil_state_quaternion_t, pitchspeed) }, \
{ "yawspeed", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_hil_state_quaternion_t, yawspeed) }, \
{ "lat", NULL, MAVLINK_TYPE_INT32_T, 0, 32, offsetof(mavlink_hil_state_quaternion_t, lat) }, \
{ "lon", NULL, MAVLINK_TYPE_INT32_T, 0, 36, offsetof(mavlink_hil_state_quaternion_t, lon) }, \
{ "alt", NULL, MAVLINK_TYPE_INT32_T, 0, 40, offsetof(mavlink_hil_state_quaternion_t, alt) }, \
{ "vx", NULL, MAVLINK_TYPE_INT16_T, 0, 44, offsetof(mavlink_hil_state_quaternion_t, vx) }, \
{ "vy", NULL, MAVLINK_TYPE_INT16_T, 0, 46, offsetof(mavlink_hil_state_quaternion_t, vy) }, \
{ "vz", NULL, MAVLINK_TYPE_INT16_T, 0, 48, offsetof(mavlink_hil_state_quaternion_t, vz) }, \
{ "ind_airspeed", NULL, MAVLINK_TYPE_UINT16_T, 0, 50, offsetof(mavlink_hil_state_quaternion_t, ind_airspeed) }, \
{ "true_airspeed", NULL, MAVLINK_TYPE_UINT16_T, 0, 52, offsetof(mavlink_hil_state_quaternion_t, true_airspeed) }, \
{ "xacc", NULL, MAVLINK_TYPE_INT16_T, 0, 54, offsetof(mavlink_hil_state_quaternion_t, xacc) }, \
{ "yacc", NULL, MAVLINK_TYPE_INT16_T, 0, 56, offsetof(mavlink_hil_state_quaternion_t, yacc) }, \
{ "zacc", NULL, MAVLINK_TYPE_INT16_T, 0, 58, offsetof(mavlink_hil_state_quaternion_t, zacc) }, \
} \
}
#endif
@@ -104,27 +104,27 @@ typedef struct __mavlink_hil_state_quaternion_t {
* @param zacc [mG] Z acceleration
* @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)
static inline uint16_t mavlink_msg_hil_state_quaternion_pack(uint16_t system_id, uint8_t component_id, mavlink_message_t* msg,
uint32_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);
_mav_put_uint32_t(buf, 0, time_usec);
_mav_put_float(buf, 20, rollspeed);
_mav_put_float(buf, 24, pitchspeed);
_mav_put_float(buf, 28, yawspeed);
_mav_put_int32_t(buf, 32, lat);
_mav_put_int32_t(buf, 36, lon);
_mav_put_int32_t(buf, 40, alt);
_mav_put_int16_t(buf, 44, vx);
_mav_put_int16_t(buf, 46, vy);
_mav_put_int16_t(buf, 48, vz);
_mav_put_uint16_t(buf, 50, ind_airspeed);
_mav_put_uint16_t(buf, 52, true_airspeed);
_mav_put_int16_t(buf, 54, xacc);
_mav_put_int16_t(buf, 56, yacc);
_mav_put_int16_t(buf, 58, zacc);
_mav_put_float_array(buf, 4, attitude_quaternion, 4);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
#else
mavlink_hil_state_quaternion_t packet;
@@ -175,28 +175,28 @@ static inline uint16_t mavlink_msg_hil_state_quaternion_pack(uint8_t system_id,
* @param zacc [mG] Z acceleration
* @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,
static inline uint16_t mavlink_msg_hil_state_quaternion_pack_chan(uint16_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)
uint32_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);
_mav_put_uint32_t(buf, 0, time_usec);
_mav_put_float(buf, 20, rollspeed);
_mav_put_float(buf, 24, pitchspeed);
_mav_put_float(buf, 28, yawspeed);
_mav_put_int32_t(buf, 32, lat);
_mav_put_int32_t(buf, 36, lon);
_mav_put_int32_t(buf, 40, alt);
_mav_put_int16_t(buf, 44, vx);
_mav_put_int16_t(buf, 46, vy);
_mav_put_int16_t(buf, 48, vz);
_mav_put_uint16_t(buf, 50, ind_airspeed);
_mav_put_uint16_t(buf, 52, true_airspeed);
_mav_put_int16_t(buf, 54, xacc);
_mav_put_int16_t(buf, 56, yacc);
_mav_put_int16_t(buf, 58, zacc);
_mav_put_float_array(buf, 4, attitude_quaternion, 4);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN);
#else
mavlink_hil_state_quaternion_t packet;
@@ -231,7 +231,7 @@ static inline uint16_t mavlink_msg_hil_state_quaternion_pack_chan(uint8_t system
* @param msg The MAVLink message to compress the data into
* @param hil_state_quaternion C-struct to read the message contents from
*/
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)
static inline uint16_t mavlink_msg_hil_state_quaternion_encode(uint16_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);
}
@@ -245,7 +245,7 @@ static inline uint16_t mavlink_msg_hil_state_quaternion_encode(uint8_t system_id
* @param msg The MAVLink message to compress the data into
* @param hil_state_quaternion C-struct to read the message contents from
*/
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)
static inline uint16_t mavlink_msg_hil_state_quaternion_encode_chan(uint16_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);
}
@@ -273,26 +273,26 @@ static inline uint16_t mavlink_msg_hil_state_quaternion_encode_chan(uint8_t syst
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
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)
static inline void mavlink_msg_hil_state_quaternion_send(mavlink_channel_t chan, uint32_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);
_mav_put_uint32_t(buf, 0, time_usec);
_mav_put_float(buf, 20, rollspeed);
_mav_put_float(buf, 24, pitchspeed);
_mav_put_float(buf, 28, yawspeed);
_mav_put_int32_t(buf, 32, lat);
_mav_put_int32_t(buf, 36, lon);
_mav_put_int32_t(buf, 40, alt);
_mav_put_int16_t(buf, 44, vx);
_mav_put_int16_t(buf, 46, vy);
_mav_put_int16_t(buf, 48, vz);
_mav_put_uint16_t(buf, 50, ind_airspeed);
_mav_put_uint16_t(buf, 52, true_airspeed);
_mav_put_int16_t(buf, 54, xacc);
_mav_put_int16_t(buf, 56, yacc);
_mav_put_int16_t(buf, 58, zacc);
_mav_put_float_array(buf, 4, 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;
@@ -338,26 +338,26 @@ static inline void mavlink_msg_hil_state_quaternion_send_struct(mavlink_channel_
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_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)
static inline void mavlink_msg_hil_state_quaternion_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint32_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);
_mav_put_uint32_t(buf, 0, time_usec);
_mav_put_float(buf, 20, rollspeed);
_mav_put_float(buf, 24, pitchspeed);
_mav_put_float(buf, 28, yawspeed);
_mav_put_int32_t(buf, 32, lat);
_mav_put_int32_t(buf, 36, lon);
_mav_put_int32_t(buf, 40, alt);
_mav_put_int16_t(buf, 44, vx);
_mav_put_int16_t(buf, 46, vy);
_mav_put_int16_t(buf, 48, vz);
_mav_put_uint16_t(buf, 50, ind_airspeed);
_mav_put_uint16_t(buf, 52, true_airspeed);
_mav_put_int16_t(buf, 54, xacc);
_mav_put_int16_t(buf, 56, yacc);
_mav_put_int16_t(buf, 58, zacc);
_mav_put_float_array(buf, 4, 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;
@@ -392,9 +392,9 @@ static inline void mavlink_msg_hil_state_quaternion_send_buf(mavlink_message_t *
*
* @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 the number.
*/
static inline uint64_t mavlink_msg_hil_state_quaternion_get_time_usec(const mavlink_message_t* msg)
static inline uint32_t mavlink_msg_hil_state_quaternion_get_time_usec(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint64_t(msg, 0);
return _MAV_RETURN_uint32_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, 4);
}
/**
@@ -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, 20);
}
/**
@@ -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, 24);
}
/**
@@ -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, 28);
}
/**
@@ -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, 32);
}
/**
@@ -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, 36);
}
/**
@@ -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, 40);
}
/**
@@ -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, 44);
}
/**
@@ -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, 46);
}
/**
@@ -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, 48);
}
/**
@@ -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, 50);
}
/**
@@ -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, 52);
}
/**
@@ -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, 54);
}
/**
@@ -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, 56);
}
/**
@@ -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, 58);
}
/**