The general results of Bradshaw and Porter (1), (2) are extended to allow for a computational time-delay of up to one sampling period by a simple modification of the control algorithms. The resulting control algorithms are simple to implement and provide tight non-interacting control. Their efficiency and effectiveness are demonstrated by the presentation of the results of a laboratory microprocessor implementation in which the controllers are required to effect fuselage pitch-pointing and vertical translation manoevres in the case of an analogue computer representation of the YF-16 aircraft. The general results of Bradshaw and Porter (1), (2) have been extended to allow for a computational time delay of up to one sampling period by a simple modification of the control algorithms. The resulting control algorithms are simple to implement and provide tight non-interacting control. Their efficiency and effectiveness have been demonstrated by the presentation of the results of a laboratory microprocessor implementation in which the controllers were required to effect fuselage pitch pointing and vertical translation manoeuvres in the case of an analogue computer representation of the YF-16 aircraft.


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    Title :

    Microprocessor implementation of fast-sampling direct digital flight-mode controllers


    Additional title:

    Einsatz eines Mikroprozessors in einem schnell samplendem, direktem digitalem Flugkontrollsystem


    Contributors:
    Porter, B. (author) / Bradshaw, A. (author) / Woodhead, M.A. (author) / Garis, A. (author)

    Published in:

    Publication date :

    1983


    Size :

    8 Seiten, 2 Bilder, 7 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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