RotatingLibrationPoint.GetSpacecraftState(Spacecraft, Variable, Variable) Method

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Description

Gets the Spacecraft object's position and velocity at the Spacecraft's current epoch in the specified frame and with respect to the specified origin.

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

RotatingLibrationPoint.GetSpacecraftState(	Spacecraft spacecraft,
	Variable frame,
	Variable origin)

Arguments

spacecraft
Description:	Spacecraft whose state will be used.

frame

Description:

The desired reference frame of the state vector.

Valid Values:

Value	Label
1	ICRF
2	Inertial MJ2000 Ecliptic
3	Non-Inertial RLP Frame

origin

Description:

The desired origin of the frame describing the state vector.

Valid Values:

Value	Label
1	Libration Point
2	System Barycenter
3	Primary System Barycenter
4	Secondary System Barycenter

Return Value

Type:

Array of number (size = 6)

The state vector, in units of km and km/s, of the Spacecraft in the desired frame.

Syntax

myArray1 = myRotatingLibrationPoint1.GetSpacecraftState(mySpacecraft1, myVariable1, myVariable2);