The research on the optimization and guidance of flight trajectories in the presence of windshear performed by the Aero-Astronautics Group of Rice University is summarized. This research refers to windshear recovery systems and covers three areas of investigation: take-off, abort landing, and penetration landing. Determination of optimal trajectories and development of near-optimal guidance schemes are outlined.


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    Title :

    Optimal trajectories and guidance trajectories for aircraft flight through windshears


    Contributors:
    Miele, A. (author)

    Conference:

    IEEE Conference on Decision and Control ; 1990 ; Honolulu, HI, United States


    Publication date :

    1990-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





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