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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>
This commit is contained in:
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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validation/module_schema.yaml
+1 -1
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@@ -147,7 +147,7 @@ parameters:
'bit/s', 'B/s',
'deg', 'deg*1e7', 'deg/s',
'celcius', 'gauss', 'gauss/s', 'mgauss', 'mgauss^2',
'hPa', 'kg', 'kg/m^2', 'kg m^2',
'hPa', 'kg', 'kg/m^2', 'kg m^2', 'kg/m^3',
'mm', 'm', 'm/s', 'm^2', 'm/s^2', 'm/s^3', 'm/s^2/sqrt(Hz)', 'm/s/rad',
'Ohm', 'V', 'A',
'us', 'ms', 's',