每年出版 6 期
ISSN 打印: 1948-2590
ISSN 在线: 1948-2604
ROBUST CONTROL DESIGN TO SUPPRESS WING ROCK MOTION OF A WIND-TUNNEL AIRCRAFT MODEL IN 3DOF GIMBALS
摘要
The dynamics of a scaled actively controlled model of a maneuverable aircraft in three degrees of freedom (3DOF) gimbals is considered. A robust control algorithm suppressing wing rock motion at high angles of attack is proposed. The robust control design is based on linear parameter varying design methods, which are an extension of H∞ optimization on linear parameter-dependent systems. Wing rock suppression with the designed control law is validated using nonlinear time-domain simulations.
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Ignatyev D. I., Vallet C., Choukroun D., Philippe C., Nebylov A., Ganet M., Neural network adaptive control of wing-rock motion of aircraft model mounted on three-degree-of-freedom dynamic rig in wind tunnel, Progress in Flight Dynamics, Guidance, Navigation, and Control – Volume 10, 2018. Crossref