飞机侧向控制系统的鲁棒稳定性设计

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1990, Vol. 11 ›› Issue (12): 610-616.

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THE DESIGN OF ROBUSTNESS STABILITY OF AIRCRAFT LATERAL CONTROL SYSTEM

Zhao Jun, Mao Jianqin

Beijing University of Aeronautics and Astronautics

Received:1989-09-28 Revised:1990-03-15 Online:1990-12-25 Published:1990-12-25

Abstract

Abstract: The Reversed-Frame-Normalizing (RFN) method is employed to analyse and design the robustness of aircraft lateral control system. In comparison with Inverse Nyquist-Array (IKA) method, the RFN method for the system could not only design the stability and dynamic performances but also provide robustness with respect to plant uncertainty. Numerical results are presented for a two-input/two-output lateral control system of a high-altitude and high-speed fighter.

Key words: multivariable, robustness, aircraft lateral control system.

Zhao Jun;Mao Jianqin. THE DESIGN OF ROBUSTNESS STABILITY OF AIRCRAFT LATERAL CONTROL SYSTEM[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1990, 11(12): 610-616.

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THE DESIGN OF ROBUSTNESS STABILITY OF AIRCRAFT LATERAL CONTROL SYSTEM

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