TwoBodyGravityGetPartialDerivativesEvaluator Method

Gets an evaluator that calculates the partial derivatives of the two body gravity acceleration with respect to any of the independentVariables parameters that apply.

Namespace: AGI.Foundation.Celestial
Assembly: AGI.Foundation.OrbitPropagation (in AGI.Foundation.OrbitPropagation.dll) Version: 24.2.419.0 (24.2.419.0)

Syntax

C++

Copy

public PartialDerivativesEvaluator GetPartialDerivativesEvaluator(
	IList<IPartialDifferentiable> independentVariables,
	EvaluatorGroup group
)

Public Function GetPartialDerivativesEvaluator ( 
	independentVariables As IList(Of IPartialDifferentiable),
	group As EvaluatorGroup
) As PartialDerivativesEvaluator

public:
virtual PartialDerivativesEvaluator^ GetPartialDerivativesEvaluator(
	IList<IPartialDifferentiable^>^ independentVariables, 
	EvaluatorGroup^ group
) sealed

abstract GetPartialDerivativesEvaluator : 
        independentVariables : IList<IPartialDifferentiable> * 
        group : EvaluatorGroup -> PartialDerivativesEvaluator 
override GetPartialDerivativesEvaluator : 
        independentVariables : IList<IPartialDifferentiable> * 
        group : EvaluatorGroup -> PartialDerivativesEvaluator

Parameters

independentVariables: Type: System.Collections.GenericIListIPartialDifferentiable
The list of IPartialDifferentiable representing the independent variables that the created partial derivative evaluator calculates partials with respect to.
group: Type: AGI.FoundationEvaluatorGroup
The evaluator group to contain the evaluator.

TwoBodyGravityAddLanguageSpecificTextSet("LST2E3110D2_0?cpp=::|nu=.");GetPartialDerivativesEvaluator Method

Parameters

Return Value

Implements

Reference

TwoBodyGravityGetPartialDerivativesEvaluator Method