Description
Converts the specified relative state from the inputSystem to the outputSystem in reference to the refSC.
Timing Precision Mode
This page describes functionality in millisecond timing precision mode.
Click here to see the documentation for this object in nanosecond timing precision mode.
Method Signature
Arguments
inputSystem
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Description:
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The coordinate system from which to convert.
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Valid Values:
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Value
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Label
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0
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Mean of J2000 Earth Equator
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1
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VNB
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2
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LVLH
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5
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UVW
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6
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RIC
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7
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LVC (Cylindrical)
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8
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RIC Cylindrical
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9
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RIC Spherical
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outputSystem
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Description:
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The coordinate system to which to convert.
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Valid Values:
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Value
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Label
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0
|
Mean of J2000 Earth Equator
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1
|
VNB
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2
|
LVLH
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5
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UVW
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6
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RIC
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7
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LVC (Cylindrical)
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8
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RIC Cylindrical
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9
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RIC Spherical
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referenceSC
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Description:
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The Spacecraft to which the reference state will be evaluated.
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state
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Description:
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Array containing the relative state to convert in the inputSystem.
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Required Size:
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6
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Return Value
Type:
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Array of number (size = 6)
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Returns the relative state converted into the outputSytem in units of km and km/s
Syntax
myArray1 = RelativeMotionUtilities.ConvertRelativeState(myVariable1, myVariable2, mySpacecraft1, myArray2);
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See also
RelativeMotionUtilities Object
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