Roman Bapst dd2322d622

Added PerformanceModel for fixed wing (#22091) ...

* 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>

2023-11-21 17:13:50 +01:00

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module_schema.yaml

Added PerformanceModel for fixed wing (#22091)

2023-11-21 17:13:50 +01:00