This paper discusses the integration of a Microwave Landing System and an Inertial Navigation System. The system is built by Lear Siegler, Inc. (LSI) for pallet installation on the USAF C-141 transport aircraft. The main emphasis of this paper is the MLS/INS integration using a constant gain filter algorithm. The system was simulated in the lab, bench tested, and later flight tested on the C-141 using the MLS facilities at Wallops Island, VA. This work was completed for the USAF/ASD under Contract F33615-85-C-3603.


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    Title :

    MLS/INS Terminal Area Navigation


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Aerospace Technology Conference and Exposition ; 1987



    Publication date :

    1987-10-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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