forked from Archive/PX4-Autopilot
27 lines
1.4 KiB
Plaintext
27 lines
1.4 KiB
Plaintext
uint64 time_ref # ekf2 reference time. This is a timestamp passed to the
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# estimator which it uses a absolute reference.
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uint64 gyro_integral_dt # gyro integration period in us
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uint64 accelerometer_integral_dt # accelerometer integration period in us
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uint64 magnetometer_timestamp # timestamp of magnetometer measurement in us
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uint64 baro_timestamp # timestamp of barometer measurement in us
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float32[3] gyro_integral_rad # integrated gyro vector in rad
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float32[3] accelerometer_integral_m_s # integrated accelerometer vector in m/s
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float32[3] magnetometer_ga # magnetometer measurement vector (body fixed NED) in ga
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float32 baro_alt_meter # barometer altitude measurement in m
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uint64 time_usec # timestamp of gps position measurement in us
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uint64 time_usec_vel # timestamp of gps velocity measurement in us
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int32 lat # Latitude in 1E-7 degrees
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int32 lon # Longitude in 1E-7 degrees
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int32 alt # Altitude in 1E-3 meters above MSL, (millimetres)
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uint8 fix_type
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float32 eph # GPS horizontal position accuracy (metres)
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float32 epv # GPS vertical position accuracy (metres)
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float32 vel_m_s # GPS ground speed, (metres/sec)
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float32 vel_n_m_s # GPS North velocity, (metres/sec)
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float32 vel_e_m_s # GPS East velocity, (metres/sec)
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float32 vel_d_m_s # GPS Down velocity, (metres/sec)
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bool vel_ned_valid # True if NED velocity is valid
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