Conversion Flight Control for Tiltrotor Aircraft via Active Disturbance Rejection Control
نویسندگان
چکیده
The tiltrotor aircraft consists of three primary flight modes, which are helicopter mode in low forward speed flight, airplane high and conversion mode. This paper presents an active disturbance rejection controller for flight. First, a dynamics model is developed verified. Then, control laws, designed via the (ADRC) sliding (SMC) techniques, proposed with uncertainties external disturbance, estimated extended state observer. Finally, simulation automatic carried out, shows effectiveness controller.
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ژورنال
عنوان ژورنال: Aerospace
سال: 2022
ISSN: ['2226-4310']
DOI: https://doi.org/10.3390/aerospace9030155