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.
Optimal trajectories and guidance trajectories for aircraft flight through windshears
IEEE Conference on Decision and Control ; 1990 ; Honolulu, HI, United States
1990-01-01
Conference paper
No indication
English
Optimal trajectories and guidance trajectories for aircraft flight through windshears
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