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.
AIRCRAFT CONTROL SYSTEMS AND METHODS USING SLIDING MODE CONTROL AND FEEDBACK LINEARIZATION
SYSTEMES ET METHODES DE COMMANDE D`AERONEF UTILISANT UN CONTROLE SLIDING MODE ET LA LINEARISATION DE REACTION
2021-03-30
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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