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autogenerated headers for rev https://github.com/mavlink/mavlink/tree/96589baa69422373b7dff63b0e906b3e767b3a1e

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PX4BuildBot
2015-08-14 21:55:31 +00:00
parent 48553b0395
commit 753b694df1
264 changed files with 1794 additions and 1794 deletions
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common/mavlink_msg_hil_state_quaternion.h
+16 -16
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@@ -4,22 +4,22 @@
typedef struct __mavlink_hil_state_quaternion_t
{
uint64_t time_usec; ///< Timestamp (microseconds since UNIX epoch or microseconds since system boot)
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; ///< Body frame roll / phi angular speed (rad/s)
float pitchspeed; ///< Body frame pitch / theta angular speed (rad/s)
float yawspeed; ///< Body frame yaw / psi angular speed (rad/s)
int32_t lat; ///< Latitude, expressed as * 1E7
int32_t lon; ///< Longitude, expressed as * 1E7
int32_t alt; ///< Altitude in meters, expressed as * 1000 (millimeters)
int16_t vx; ///< Ground X Speed (Latitude), expressed as m/s * 100
int16_t vy; ///< Ground Y Speed (Longitude), expressed as m/s * 100
int16_t vz; ///< Ground Z Speed (Altitude), expressed as m/s * 100
uint16_t ind_airspeed; ///< Indicated airspeed, expressed as m/s * 100
uint16_t true_airspeed; ///< True airspeed, expressed as m/s * 100
int16_t xacc; ///< X acceleration (mg)
int16_t yacc; ///< Y acceleration (mg)
int16_t zacc; ///< Z acceleration (mg)
uint64_t time_usec; /*< Timestamp (microseconds since UNIX epoch or microseconds since system boot)*/
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; /*< Body frame roll / phi angular speed (rad/s)*/
float pitchspeed; /*< Body frame pitch / theta angular speed (rad/s)*/
float yawspeed; /*< Body frame yaw / psi angular speed (rad/s)*/
int32_t lat; /*< Latitude, expressed as * 1E7*/
int32_t lon; /*< Longitude, expressed as * 1E7*/
int32_t alt; /*< Altitude in meters, expressed as * 1000 (millimeters)*/
int16_t vx; /*< Ground X Speed (Latitude), expressed as m/s * 100*/
int16_t vy; /*< Ground Y Speed (Longitude), expressed as m/s * 100*/
int16_t vz; /*< Ground Z Speed (Altitude), expressed as m/s * 100*/
uint16_t ind_airspeed; /*< Indicated airspeed, expressed as m/s * 100*/
uint16_t true_airspeed; /*< True airspeed, expressed as m/s * 100*/
int16_t xacc; /*< X acceleration (mg)*/
int16_t yacc; /*< Y acceleration (mg)*/
int16_t zacc; /*< Z acceleration (mg)*/
} mavlink_hil_state_quaternion_t;
#define MAVLINK_MSG_ID_HIL_STATE_QUATERNION_LEN 64