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* created a Performance Model for fixed wing vehicle - added compensation for maximum climbrate, minimum sinkrate, minimum airspeed and trim airspeed based on weight ratio and air density - added atmosphere lib to standard atmosphere calculations --------- Signed-off-by: RomanBapst <bapstroman@gmail.com> Co-authored-by: Thomas Stastny <thomas.stastny@auterion.com>
16 lines
728 B
Plaintext
16 lines
728 B
Plaintext
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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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uint32 baro_device_id # unique device ID for the selected barometer
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float32 baro_alt_meter # Altitude above MSL calculated from temperature compensated baro sensor data using an ISA corrected for sea level pressure SENS_BARO_QNH.
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float32 baro_temp_celcius # Temperature in degrees Celsius
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float32 baro_pressure_pa # Absolute pressure in Pascals
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float32 rho # air density
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float32 eas2tas # equivalent airspeed to true airspeed conversion factor
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uint8 calibration_count # Calibration changed counter. Monotonically increases whenever calibration changes.
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