Research output: Contribution to journal › Conference article › peer-review
In the paper a flight control system for a piloted aircraft on the pitch angle is considered, taking into account the rate saturation of the aircraft controlling surface. To prevent occurrence of the non-linear pilot-involved oscillations (PIO), a nonlinear correcting device is introduced into the control loop. On the basis of the pilot's adaptation to control tasks variations, his/her mathematical model parameters are optimized and the choice of the nonlinear correcting device parameters is proposed. The sensitivity functions of the non-linear system are calculated for harmonic and square-wave reference signals. The results of the optimized system simulations are presented demonstrating good performance of the closed-loop system with nonlinear correction.
Original language | English |
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Article number | 012055 |
Journal | Journal of Physics: Conference Series |
Volume | 1864 |
Issue number | 1 |
DOIs | |
State | Published - 1 May 2021 |
Event | 13th Multiconference on Control Problems, MCCP 2020: Математическая теория управления и ее приложения (МТУиП) - ГНЦ РФ АО «Концерн «ЦНИИ «Электроприбор», Санкт-Петербург, Russian Federation Duration: 6 Oct 2020 → 8 Oct 2020 Conference number: 13 http://www.elektropribor.spb.ru/nauchnaya-deyatelnost/xiii-mkpu/index3.php |
ID: 86489041