KalmanFilterOD Object

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Description

The KalmanFilterOD object provides algorithms for performing Orbit Determination and State Estimation using a Kalman filter technique.  This allows observations to be processed sequentially, and potentially in real-time.  The sequential nature of the Kalman filter provides significant power and flexibility by allowing the user to manipulate settings interactively inside the estimation process. See the Orbit Determination Guide for more information.

 

Inheritance Hierarchy: Object->ODEstimationProcess->SequentialFilter->KalmanFilterOD

Derived Types: UnscentedKalmanFilterOD

 

Available In Editions:

Mission

 

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.

 

Properties

 

Methods

 

Deprecated Methods

 

 

See also

Orbit Determination Guide