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: 24.3.420.0 (24.3.420.0)

Syntax

C++

Copy

public Vector GetAccelerationVector()

Public Function GetAccelerationVector As Vector

public:
Vector^ GetAccelerationVector()

member GetAccelerationVector : unit -> Vector

Return Value

Type: Vector
A Vector representing the Newtonian inertial acceleration.

Reference

PropagationNewtonianPoint Class

AGI.Foundation.Propagators Namespace

PropagationNewtonianPointAddLanguageSpecificTextSet("LSTD986D1C1_0?cpp=::|nu=.");GetAccelerationVector Method

Return Value

Reference

PropagationNewtonianPointGetAccelerationVector Method