The suitability of strapdown inertial systems in providing highly reliable short-term navigation for vertical take-off and landing (VTOL) aircraft operating in an intra-urban setting under all-weather conditions was assessed. A preliminary design configuration of a skewed sensor inertial reference system employing a redundancy management concept to achieve fail-operational, fail-operational performance, was developed.


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    Title :

    Strapdown System Redundancy Management Flight Demonstration


    Publication date :

    1978


    Size :

    73 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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