Results of flight tests of the Strapdown Inertial Reference Unit (SIRU) navigation system are presented. The fault tolerant SIRU navigation system features a redundant inertial sensor unit and dual computers. System software provides for detection and isolation of inertial sensor failures and continued operation in the event of failures. Flight test results include assessments of the system's navigational performance and fault tolerance. Performance shortcomings are analyzed.


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    Title :

    Flight Test Results of the Strapdown Hexad Inertial Reference Unit (SIRU). Volume 2: Test Report


    Contributors:

    Publication date :

    1977


    Size :

    96 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English