forked from Archive/PX4-Autopilot
24 lines
1.4 KiB
Plaintext
24 lines
1.4 KiB
Plaintext
uint64 timestamp # time since system start (microseconds)
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uint64 timestamp_sample # the timestamp of the raw data (microseconds)
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float32 windspeed_north # Wind component in north / X direction (m/sec)
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float32 windspeed_east # Wind component in east / Y direction (m/sec)
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float32 variance_north # Wind estimate error variance in north / X direction (m/sec)**2 - set to zero (no uncertainty) if not estimated
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float32 variance_east # Wind estimate error variance in east / Y direction (m/sec)**2 - set to zero (no uncertainty) if not estimated
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float32 tas_innov # True airspeed innovation
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float32 tas_innov_var # True airspeed innovation variance
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float32 tas_scale # Estimated true airspeed scale factor
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float32 beta_innov # Sideslip measurement innovation
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float32 beta_innov_var # Sideslip measurement innovation variance
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uint8 source # source of wind estimate
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uint8 SOURCE_EKF = 0 # wind estimate source is the EKF
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uint8 SOURCE_AS_BETA_ONLY = 1 # wind estimate from airspeed selector, only based on synthetic sideslip fusion
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uint8 SOURCE_AS_SENSOR_1 = 2 # combined synthetic sideslip and airspeed fusion (data from first airspeed sensor)
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uint8 SOURCE_AS_SENSOR_2 = 3 # combined synthetic sideslip and airspeed fusion (data from second airspeed sensor)
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uint8 SOURCE_AS_SENSOR_3 = 4 # combined synthetic sideslip and airspeed fusion (data from third airspeed sensor)
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