RotatingLibrationPoint.SetSpacecraftState(Spacecraft, Variable, Variable, Array) Method

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Description

Sets the Spacecraft object's position and velocity at the Spacecraft's current epoch given the state vector 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.SetSpacecraftState(	Spacecraft spacecraft,
	Variable frame,
	Variable origin,
	Array posVelArray)

Arguments

spacecraft
Description:	Spacecraft whose state will be set.

frame

Description:

The reference frame of the state vector.

Valid Values:

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

origin

Description:

The 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

posVelArray
Description:	The state vector containing the position and velocity which will be applied to the Spacecraft object.
Required Size:	6

Syntax

myRotatingLibrationPoint1.SetSpacecraftState(mySpacecraft1, myVariable1, myVariable2, myArray1);