SpacecraftODProperties.ElementSetToProcess Property

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Description

Indicates the element set to use when estimating the orbit state. Changing this value will reinitialize the process noise matrix to a diagonal matrix in the ICRF 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.

 

Attributes

Type:

string

Access:

read

Valid Values:

Value

Label

"Cartesian"

Cartesian Elements

"Equinoctial"

Equinoctial Elements

"Undefined"

No Orbit State Elements

 

Syntax

myString1 = mySpacecraftODProperties1.ElementSetToProcess;

 

See also

SpacecraftODProperties Object

Defining the Element Set to Process

Orbit Determination Guide