2019
DOI: 10.32620/reks.2017.4.06
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Cинтез Робастного Під-Регулятора Для Невизначеної Нелінійної Моделі Бпла З Використанням Штучної Моделі Посилення І Тимчасової Затримки

Фархади Рахман Мохаммади,
Вячеслав Иванович Кортунов

Abstract: Estimations of the flight vehicles aerodynamic coefficients through the theoretical, numerical, wind tunnel and flight-test methods have always errors and uncertainties. Nonlinear dynamics of the unmanned aerial vehicle due to speed variations, as well as variability and uncertainty of the aerodynamic coefficients can be considered as an uncertain model. A robust proportional-integral-derivative controller is designed based on the nonlinear optimization in the time domain for the uncertain nonlinear dynamical … Show more

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