高超声速变外形飞行器事件触发有限时间控制

doi:10.7527/S1000-6893.2023.28494

Abstract

Abstract:

This paper proposes a novel event-triggered fast finite time sliding mode control for the hypersonic vehicle with frequent actuator deflection in the morphing phase. The original model of the hypersonic morphing vehicle is transformed into the control-oriented model， which is employed in the controller design. The fast finite time control theory is adopted to develop a control system for the hypersonic morphing phase. The switching dynamic event-triggering mechanism is introduced to reduce the frequency of actuator deflection. Meanwhile， the possible performance loss is fully considered in the procedure. The Lyapunov theory is utilized to prove the stability of the closed-loop system and the convergence of the tracking error. Compared with conventional finite-time control methods， fast finite-time control enhances the convergence rate when the system state is far from the equilibrium point. Furthermore， the event-triggering mechanism effectively reduces the frequency of actuating the actuator without obvious performance loss. Simulation verifies the effectiveness and excellent performance of the controller proposed.

Key words: hypersonic morphing vehicle, attitude control, finite time control, sliding mode control, switching event-triggering mechanism, dynamic event-triggering mechanism

CLC Number:

V448

Hao ZHANG, Peng WANG, Guojian TANG, Weimin BAO. Event-triggered fast finite time control for hypersonic morphing vehicles[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(15): 528494.

Figures/Tables 14

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References 28

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方法	攻角α/（°）	侧滑角β/（°）	倾侧角γ _V/（°）
FTETM	0.04	-0.050	0
RTETM	-0.05	-0.390	-0.130
SETM	0.03	-0.063	-0.001
SDETM	0.03	-0.060	-0.001

方法	俯仰通道/次	偏航通道/次	滚转通道/次
FTETM	741	608	368
RTETM	403	284	266
SETM	584	461	334
SDETM	521	391	284

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Event-triggered fast finite time control for hypersonic morphing vehicles

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