PropagationEulerianAxes.GetDerivatives Method

This is used by the NumericalPropagatorDefinition to obtain an instance of a state element evaluator that can compute the derivatives of this element of the state during propagation. It cannot be used outside of a NumericalPropagator as the geometry for the propagation state will be unavailable.

Namespace: AGI.Foundation.Propagators
Assembly: AGI.Foundation.OrbitPropagation (in AGI.Foundation.OrbitPropagation.dll) Version: 25.1.421.0 (25.1.421.0)

Syntax

C++

Copy

public override PropagationStateElementEvaluator GetDerivatives(
	EvaluatorGroup group
)

Public Overrides Function GetDerivatives ( 
	group As EvaluatorGroup
) As PropagationStateElementEvaluator

public:
virtual PropagationStateElementEvaluator^ GetDerivatives(
	EvaluatorGroup^ group
) override

abstract GetDerivatives : 
        group : EvaluatorGroup -> PropagationStateElementEvaluator 
override GetDerivatives : 
        group : EvaluatorGroup -> PropagationStateElementEvaluator

Parameters

group: Type: AGI.Foundation.EvaluatorGroup
The group in which to create the evaluator and its dependents.

Return Value

Type: PropagationStateElementEvaluator
The evaluator that can compute the derivatives of this element of the state.

Reference

PropagationEulerianAxes Class

AGI.Foundation.Propagators Namespace

PropagationEulerianAxes.AddLanguageSpecificTextSet("LSTAC86B6F9_0?cpp=::|nu=.");GetDerivatives Method

Parameters

Return Value

Reference

PropagationEulerianAxes.GetDerivatives Method