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    Quality control in integrated navigation systems

    Access Status
    Fulltext not available
    Authors
    Teunissen, Peter
    Date
    1990
    Type
    Journal Article
    
    Metadata
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    Citation
    Teunissen, P.J.G. 1990. Quality control in integrated navigation systems. IEEE Aerospace and Electronic Systems Magazine. 7 (5): pp. 35-41.
    School
    Department of Spatial Sciences
    URI
    http://hdl.handle.net/20.500.11937/44715
    Collection
    • Curtin Research Publications
    Abstract

    Real-time estimation of parameters in dynamic systems becomes increasingly important in the field of high precision navigation. The real-time estimation inevitably requires real-time testing of the models underlying the navigation system. This paper presents: 1. A real-time recursive testing procedure that can be used in conjunction with the well-known Kalman filter algorithm: 2. Diagnostic tools for inferring the detectability of particular model errors. The testing procedure consists of three steps: detection, identification and adaptation. It can accomodate model errors in both the measurement model and dynamic model of the integrated navigation system. The tests proposed are optimal in the uniformly-most-powerful-invariant sense.

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