Package | Description |
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fr.cnes.sirius.patrius.assembly.models |
Constructor and Description |
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AeroModel(Assembly inAssembly,
Atmosphere inAtmosphere,
OneAxisEllipsoid inGeodPos)
Aero model (the acceleration is computed from all the sub parts of the vehicle)
with default step for finite differences computation.
|
AeroModel(Assembly inAssembly,
Atmosphere inAtmosphere,
OneAxisEllipsoid earthShapeIn,
double altStep)
Aero model (the acceleration is computed from all the sub parts of the vehicle)
with an
Atmosphere model and a OneAxisEllipsoid for acceleration partial
derivatives computation with respect to state by finite differences(including density
partial derivatives). |
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