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PropagationEulerianAxesIntegrationAxes Property

Gets a Axes which is parameterized on the attitude and angular velocity in the state during integration. This axes is only valid while the NumericalPropagator is running. For more general use, a AxesInterpolator or a RotationalMotionInterpolator should be created from the NumericalPropagationStateHistory produced by the propagator.

Namespace:  AGI.Foundation.Propagators
Assembly:  AGI.Foundation.OrbitPropagation (in AGI.Foundation.OrbitPropagation.dll) Version: 22.2.414.0 (22.2.414.0)
Syntax
public Axes IntegrationAxes { get; }

Property Value

Type: Axes
See Also