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 nanosecond timing precision mode.

Click here to see the documentation for this object in millisecond 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);

 

 

See also

SpacecraftProcessNoise Object

SpacecraftProcessNoise.SetProcessNoiseInFrame