An aircraft terminal area landing approach system based upon the Discrete Tracking Problem of Optimal Control Theory is presented. The control vector is made up of the aircraft's thrust and flight path. An example of the landing approach system will be presented.
Aicraft terminal area guidance based on the discrete tracking problem of optimal control theory
Bordterminal fuer Gelaendelenkung basierend auf dem diskreten Nachfuehrproblem der optimalen Steuertheorie
Conf. Proc. IEEE Southeastcon '84 ; 399-402
1984
4 Seiten, 7 Quellen
Aufsatz (Konferenz)
Englisch
FLUGZEUG , FLUGREGELUNG , BORDRECHNER , LANDEVERFAHREN , STEUERUNG , VEKTOR , SCHUBKRAFT
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