IersTechnicalNote36RelativisticCorrectionForceRouthsRuleAngularMomentumPerUnitMass Method

A static helper method that computes a CentralBodyAngularMomentumPerUnitMass vector for the input centralBody. This method uses Routh's rule for an ellipsoid coupled with the angular velocity vector computed between the fixed and inertial frames defined on the centralBody.

Namespace: AGI.Foundation.Celestial
Assembly: AGI.Foundation.OrbitPropagation (in AGI.Foundation.OrbitPropagation.dll) Version: 24.3.420.0 (24.3.420.0)

Syntax

C++

Copy

public static Vector RouthsRuleAngularMomentumPerUnitMass(
	CentralBody centralBody
)

Public Shared Function RouthsRuleAngularMomentumPerUnitMass ( 
	centralBody As CentralBody
) As Vector

public:
static Vector^ RouthsRuleAngularMomentumPerUnitMass(
	CentralBody^ centralBody
)

static member RouthsRuleAngularMomentumPerUnitMass : 
        centralBody : CentralBody -> Vector

Parameters

centralBody: Type: AGI.Foundation.CelestialCentralBody
The central body for which to create this vector.

Return Value

Type: Vector
A vector suitable for use with the CentralBodyAngularMomentumPerUnitMass property.

Reference

IersTechnicalNote36RelativisticCorrectionForce Class

AGI.Foundation.Celestial Namespace

IersTechnicalNote36RelativisticCorrectionForceAddLanguageSpecificTextSet("LST6D1F66AE_0?cpp=::|nu=.");RouthsRuleAngularMomentumPerUnitMass Method

Parameters

Return Value

Reference

IersTechnicalNote36RelativisticCorrectionForceRouthsRuleAngularMomentumPerUnitMass Method