Methods and systems for controlling a bank angle, a heading angle and an altitude of an aircraft during flight are provided. The methods and systems disclosed herein make use of sliding mode control and feedback linearization control (nonlinear dynamic control) techniques. The methods and systems can provide autopilot-type functions that can autonomously execute aggressive maneuvers as well as more gentle maneuvers for aircraft.


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    Title :

    AIRCRAFT CONTROL SYSTEMS AND METHODS USING SLIDING MODE CONTROL AND FEEDBACK LINEARIZATION


    Additional title:

    SYSTEMES ET METHODES DE COMMANDE D`AERONEF UTILISANT UN CONTROLE SLIDING MODE ET LA LINEARISATION DE REACTION


    Contributors:

    Publication date :

    2021-03-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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