SpacecraftODProperties.SGP4STMPerturbationPct Property

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Description

Size of the perturbation to apply in computing the state transition matrix for SGP4 state estimation as a percentage of the a priori state property value.

 

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.

 

Attributes

Type:

number

Access:

read/write

Default Value:

0.00001

Valid Range:

SpacecraftODProperties.SGP4STMPerturbationPct > 0

 

Syntax

myVariable1 = mySpacecraftODProperties1.SGP4STMPerturbationPct;

 

mySpacecraftODProperties1.SGP4STMPerturbationPct = myVariable1;

 

See also

SpacecraftODProperties Object

Orbit Determination Guide