RelativeMotionUtilities.ConvertRelativeState(Variable, Variable, Spacecraft, Array) Method

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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. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode.

Click here to see the documentation for this object in nanosecond timing precision mode.

Method Signature

RelativeMotionUtilities.ConvertRelativeState(	Variable inputSystem,
	Variable outputSystem,
	Spacecraft referenceSC,
	Array state)

Arguments

inputSystem

Description:

The coordinate system from which to convert.

Valid Values:

Value	Label
0	ICRF
1	VNB
2	LVLH
5	UVW
6	RIC
7	LVC (Cylindrical)
8	RIC Cylindrical
9	RIC Spherical

outputSystem

Description:

The coordinate system to which to convert.

Valid Values:

Value	Label
0	ICRF
1	VNB
2	LVLH
5	UVW
6	RIC
7	LVC (Cylindrical)
8	RIC Cylindrical
9	RIC Spherical

referenceSC
Description:	The Spacecraft to which the reference state will be evaluated.

state
Description:	Array containing the relative state to convert in the inputSystem.
Required Size:	6

Return Value

Type:

Array of number (size = 6)

Returns the relative state converted into the outputSytem in units of km and km/s

Syntax

myArray1 = RelativeMotionUtilities.ConvertRelativeState(myVariable1, myVariable2, mySpacecraft1, myArray2);