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(
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String elementSetToProcess,
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Variable convertFromActiveSet)
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Arguments
elementSetToProcess
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Description:
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Element set to use in the estimation process.
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Valid Values:
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Value
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Label
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"Undefined"
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No Orbit State Elements
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"Cartesian"
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Cartesian Elements
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"Equinoctial"
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Equinoctial Elements
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convertFromActiveSet
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Description:
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Flag indicating whether or not to initialize the newly active covariance from the previously initialized set. Note: if the full covariance includes non-orbit state terms, the correlations between those and the orbit state are set to zero after this call.
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Valid Values:
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Value
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Label
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0
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false
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1
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true
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Syntax
mySpacecraftODProperties1.SetElementSetToProcess(myString1, myVariable1);
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See also
SpacecraftODProperties Object
SpacecraftODProperties.SetElementSetToProcess
Orbit Determination Guide
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