SpacecraftProcessNoise.SetProcessNoiseInFrame(String, Matrix) Method

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Description

Sets the process noise rate matrix of the spacecraft state in the specified attitude reference frame.

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

SpacecraftProcessNoise.SetProcessNoiseInFrame(	String inputReferenceFrame,
	Matrix inputProcessNoise)

Arguments

inputReferenceFrame

Description:

The attitude reference frame of the input process noise rate matrix.

Valid Values:

Value	Label
"ICRF"	ICRF
"VNB"	VNB
"LVLH"	LVLH
"GEODETIC"	GEODETIC
"UVW"	UVW
"RIC"	RIC

inputProcessNoise
Description:	The input process noise rate matrix, in the user-specfied attitude reference frame.

Syntax

mySpacecraftProcessNoise1.SetProcessNoiseInFrame(myString1, myMatrix1);