SpacecraftODProperties.SetElementSetToProcess(String) Method

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Description

Sets the orbit state element set to use in the estimation process, and optionally converts the covariance from the active set.

 

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

SpacecraftODProperties.SetElementSetToProcess(

String elementSetToProcess)

 

 

Arguments

elementSetToProcess


Description:

Element set to use in the estimation process.

Valid Values:

Value

Label

"Undefined"

No Orbit State Elements

"Cartesian"

Cartesian Elements

"Equinoctial"

Equinoctial Elements

 

 

 

 

Syntax

mySpacecraftODProperties1.SetElementSetToProcess(myString1);

 

 

See also

SpacecraftODProperties Object

SpacecraftODProperties.SetElementSetToProcess

Orbit Determination Guide