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uint64_t | time_usec |
| | Timestamp (microseconds since UNIX epoch or microseconds since system boot)
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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)
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float | rollspeed |
| | Body frame roll / phi angular speed (rad/s)
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float | pitchspeed |
| | Body frame pitch / theta angular speed (rad/s)
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| |
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float | yawspeed |
| | Body frame yaw / psi angular speed (rad/s)
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int32_t | lat |
| | Latitude, expressed as * 1E7.
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int32_t | lon |
| | Longitude, expressed as * 1E7.
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int32_t | alt |
| | Altitude in meters, expressed as * 1000 (millimeters)
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int16_t | vx |
| | Ground X Speed (Latitude), expressed as m/s * 100.
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int16_t | vy |
| | Ground Y Speed (Longitude), expressed as m/s * 100.
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int16_t | vz |
| | Ground Z Speed (Altitude), expressed as m/s * 100.
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|
uint16_t | ind_airspeed |
| | Indicated airspeed, expressed as m/s * 100.
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| |
|
uint16_t | true_airspeed |
| | True airspeed, expressed as m/s * 100.
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| |
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int16_t | xacc |
| | X acceleration (mg)
|
| |
|
int16_t | yacc |
| | Y acceleration (mg)
|
| |
|
int16_t | zacc |
| | Z acceleration (mg)
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| |
The documentation for this struct was generated from the following file:
1.8.9.1
