重型运载火箭预设时间自适应控制

doi:10.12305/j.issn.1001-506X.2023.08.32

Abstract

Abstract:

In view of the attitude control problem of the heavy-lift launch vehicle with model uncertainty and unknown external interference, a novel predefined-time adaptive control method is proposed, which makes the convergence time of attitude control errors is independent of any system initial condition and can be preset. Firstly, a novel predefined-time sliding mode surface is designed, and the sliding mode surface switching method is used to avoid the singularity. Secondly, a predefined-time sliding mode controller is designed. The lumped disturbance of the system is estimated by neural network and compensated in the controller, and the adaptive law is designed to adaptively adjust the weight coefficient of neural network. The predefined-time stability of the designed controller is proved based on Lyapunov stability theorem. Finally, the feasibility and effectiveness of the proposed method is verified by numerical simulations.

Key words: heavy-lift launch vehicle, predefined-time sliding mode surface, predefined-time sliding mode control, neural network, adaptive law

CLC Number:

V525

Yushi JIANG, Yang CHEN, Lu GAO, Ligen CAI, Jixing LYU. Predefined-time adaptive control for heavy-lift launch vehicles[J]. Systems Engineering and Electronics, 2023, 45(8): 2570-2577.

Figures/Tables 13

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References 31

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组成项	参数值
滑模面	γ₁=7, γ₂=9, ε=0.01
控制器	$\tilde{p}=0.9$, μ=0.5, k=1.2, h=0.8, κ=2

对比控制器	参数值
FTC	λ_m=2, k_m2=2, k_m3=2, k_m3=1, k_m4=1, q_n1=9, p_n1=7, q_n2=9, p_n2=5, a_n1=2
FxTC	a_n2=1, λ_n=8, m_n1=9, n_n1=5, m_n2=5, n_n2=3, b_n1=2, b_n2=1, τ_n=0.1

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Predefined-time adaptive control for heavy-lift launch vehicles

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