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Added PerformanceModel for fixed wing (#22091)

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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


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Signed-off-by: RomanBapst <bapstroman@gmail.com>
Co-authored-by: Thomas Stastny <thomas.stastny@auterion.com>
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Roman Bapst
2023-11-21 17:13:50 +01:00
committed by GitHub
co-authored by Thomas Stastny
parent 70cd224236
commit dd2322d622
40 changed files with 800 additions and 474 deletions
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msg/VehicleAirData.msg
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@@ -10,5 +10,6 @@ float32 baro_temp_celcius # Temperature in degrees Celsius
float32 baro_pressure_pa # Absolute pressure in Pascals
float32 rho # air density
float32 eas2tas # equivalent airspeed to true airspeed conversion factor
uint8 calibration_count # Calibration changed counter. Monotonically increases whenever calibration changes.