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PropagationNewtonianPointGetAccelerationVector Method

Gets a Vector representing the acceleration according to Newton's second law of motion in the given inertial IntegrationFrame.

When using partial derivatives (such as using a StateTransitionMatrix to calculate covariance over time) note that the PropagationNewtonianPoint itself is the IPartialDifferentiable which represents the partials of the acceleration, not the Vector returned by this method.

Namespace:  AGI.Foundation.Propagators
Assembly:  AGI.Foundation.OrbitPropagation (in AGI.Foundation.OrbitPropagation.dll) Version: 22.2.414.0 (22.2.414.0)
Syntax
public Vector GetAccelerationVector()

Return Value

Type: Vector
A Vector representing the Newtonian inertial acceleration.
See Also