The acceleration in meters/second^2
contribution of the indicated Type, returned as cartesian
components in the specified frame.
| [Visual Basic .NET] |
|---|
Public Sub GetAcceleration( _
ByVal Type As AgEAccelType, _
ByVal Frame As AgEUtFrame, _
ByRef X As Double, _
ByRef Y As Double, _
ByRef Z As Double _
)
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| [C#] |
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public void GetAcceleration(
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| [Managed C++] |
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public: void GetAcceleration(
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| [Java] |
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public getAcceleration(
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| [Unmanaged C++] |
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public: HRESULT GetAcceleration(
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- Type
-
Acceleration type (i.e., a constituent of the force model)Member Value Description eTotalAccel 0 Total accleration. eTwoBodyAccel 1 Two body contribution. eGravityAccel 2 Contribution of the total gravity field. ePerturbedGravityAccel 3 Contribution of the total gravity field minus the two body contribution. eSolidTidesAccel 4 Contribution of solid tides. Will be zero if the force model is not set to consider this effect. eOceanTidesAccel 5 Contribution of ocean tides. Will be zero if the force model is not set to consider this effect. eDragAccel 6 Contribution of atmospheric drag. Will be zero if the force model is not set to consider this effect. eSRPAccel 7 Contribution of solar radiation pressure. Will be zero if the force model is not set to consider this effect. eThirdBodyAccel 8 Contribution of all third bodies. Will be zero if the force model is not considering any third body forces. eGenRelativityAccel 9 Contribution of general relativity effects. Will be zero if the force model is not set to consider this effect. eAddedAccel 10 Contribution of any additional acceleration, say by a plugin. eAlbedoAccel 11 Contribution of albedo (reflected solar radiation pressure). eThermalRadiationPressureAccel 12 Contribution of thermal radiation pressure. - Frame
-
Requested frame to express the resultsMember Value Description eUtFrameInertial 0 eUtFrameFixed 1 eUtFrameLVLH 2 eUtFrameNTC 3 eUtFrameICRF 4 eUtFrameJ2000 5 - X
- X component of the acceleration contribution in requested frame
- Y
- Y component of the acceleration contribution in requested frame
- Z
- Z component of the acceleration contribution in requested frame