The loss of an aircraft's primary flight controls can lead to a fatal accident. However, if the engine thrust is available, controllability and safety can be retained. A flight control is described using engine thrust only when an aircraft has lost all primary flight controls. This is a kind of flight control reconfiguration. For safe return, the aircraft must first descend to a landing area, decelerate to a landing speed, and then be capable of precise flight control for approach and landing. For these purposes, two kinds of controllers are required: a controller for descent and deceleration and a controller for approach and landing. The former controller is designed for longitudinal motion using a model-following control method, based on a linear quadratic regulator. The latter is designed by an H infinity state-feedback control method for both longitudinal and lateral-directional motions. Computer simulation is conducted using linear models of the Boeing 747. The results indicate that flight path control, including approach and landing, is possible using thrust only; however, speed control proves more difficult. However, if the horizontal stabilizer is available, the airspeed can be reduced to a safe landing speed.


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    Titel :

    Flight control system design for propulsion-controlled aircraft


    Weitere Titelangaben:

    Entwurf einer Flugregelung für ein Flugzeug mit Triebwerk


    Beteiligte:
    Ochi, Y. (Autor:in)


    Erscheinungsdatum :

    2005


    Format / Umfang :

    13 Seiten, 20 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch






    Longitudinal Flight Control System Design for Propulsion Controlled Aircraft

    Ochi, Y. / Kanai, K. / International Federation of Automatic Control | British Library Conference Proceedings | 2002