共轴高速直升机增益自适应多模式切换控制

doi:10.7527/S1000-6893.2023.29088

Abstract

Abstract:

To solve the problem of nonlinear strong-coupling multi-mode switching stability control of coaxial twin-rotor high-speed helicopter， a average dwell time switching control strategy is proposed based on gain adaptivity. According to the dynamic model of coaxial high-speed helicopter， the control characteristics of its rudder surface are analyzed，and a multi-mode gain adaptive switching control structure is constructed. A non-affine nonlinear small gain high frequency filter adaptive law is proposed. The uncertainty of multi-mode switching is quickly compensated and high-frequency noise is reduced to ensure the steady-state and transient-state performance of the system. Then， a switching submodel set with uncertainties is established， and the average dwell time switching control law is designed based on adaptive gain. The control stability of the closed-loop system is proved based on the small gain theorem and Lyapunov stability theory， which ensures the stable switching control of the coaxial high-speed helicopter in low-speed-transition-high-speed full mode. Finally， a comparison with the existing control methods verifies the feasibility and effectiveness of the proposed control strategy.

Key words: coaxial high-speed helicopter, nonlinear small gain, adaptive control, average dwell time, switching control

CLC Number:

V249.121

Fengying ZHENG, Zhimin SHEN, Yaqin LI, Kaizhao XU, Xinhua WANG. Gain adaptive multi-mode switching control for coaxial high-speed helicopter[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529088.

Figures/Tables 20

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Gain adaptive multi-mode switching control for coaxial high-speed helicopter

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