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 --------- 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