Results are presented from the configuration performance study phase of the Helicopter Integrated Navigation System project. A configuration assessment is presented including processor selection, and a discussion of system architecture and configuration tradeoffs leading to a recommended configuration. Results of the system error analysis and the Kalman filter design are presented demonstrating integrated system performance.


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    Title :

    Configuration Design of a Helicopter Integrated Navigation System


    Contributors:
    S. I. Fingerote (author) / D. B. Reid (author) / D. F. Liang (author) / L. Vallot (author) / C. Greene (author)

    Publication date :

    1987


    Size :

    9 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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