SpacecraftODProperties.SetElementSetToProcess 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 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.

 

Overload List

Signatures

Return Value

Description

SpacecraftODProperties.SetElementSetToProcess(String elementSetToProcess)

None

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

SpacecraftODProperties.SetElementSetToProcess(String elementSetToProcess, Variable convertFromActiveSet)

None

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

 

 

See also

SpacecraftODProperties Object

Defining the Element Set to Process

Orbit Determination Guide