高超声速飞行器预定时间量化容错协同控制

doi:10.12305/j.issn.1001-506X.2026.05.28

Abstract

Abstract:

Aiming at the cooperative control problem of six degrees of freedom（6-DOF） hypersonic vehicle with actuator faults and signal quantization, a predetermined time quantization fault-tolerant controller is designed. Firstly, the 6-DOF hypersonic vehicle model is decomposed into position subsystem, velocity subsystem, and attitude subsystem on the time-scale, and a control-oriented model is established by combining the quantization model and the faults model. Secondly, pre-defined time controllers are designed for the three subsystems to ensure that the hypersonic vehicle completes the formation flight within the pre-defined time. An adaptive tracking method is designed to compensate for the effects of faults and signal quantization. Finally, the stability of the closed-loop system is rigorously proved based on Lyapunov theory, and the effectiveness of the controller is verified by simulation.

Key words: hypersonic vehicle, cooperative control, fault-tolerant control, pre-defined time control, quantization

CLC Number:

V 448

Jie WANG, Xiaoxuan SUN, Qing LI, Hao LU. Pre-defined time quantization fault-tolerant cooperative control for hypersonic vehicle[J]. Systems Engineering and Electronics, 2026, 48(5): 1728-1737.

Figures/Tables 12

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References 31

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参数	飞行器1	飞行器2	飞行器3
$y$/m	28000	25000	27000
$z$/m	0	−2500	3000
速度/（m·s⁻¹）	1800	1820	1780
攻角/（$^\circ $）	5	5	5

参数	数值
$p$	2/13
$q$	4/13
$ \eta $	0.25
${c_1}$	30
${\gamma _1}$	30
${\gamma _2}$	30
${\sigma _1}$	0.75
${\sigma _2}$	0.75
${c_2}$	0.1
${c_3}$	12
${\gamma _3}$	15
${\gamma _4}$	15
${\sigma _3}$	0.5
${\sigma _4}$	0.5
$ {\eta _1} $	0.09

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Pre-defined time quantization fault-tolerant cooperative control for hypersonic vehicle

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