基于观测器的再入飞行器有限时间滑模控制

IF 2.2 Q3 COMPUTER SCIENCE, CYBERNETICS
X. Liu, Xiaohuan Ren, Y. Sheng
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引用次数: 0

摘要

目的:针对具有参数不确定性和扰动的再入飞行器姿态跟踪控制问题,设计了一种基于扰动观测器的有限时间全局滑模控制方案。设计/方法/方法-首先引入反馈线性化将车辆模型转化为三个独立的二阶不确定子系统。然后,在同质性理论的基础上,提出了标称系统的有限时间控制器。在此基础上,介绍了含扰动车辆的积分滑模方法。将有限时间控制方法与积分滑模策略相结合,实现了系统的有限时间收敛,并保证了系统的全局鲁棒性。此外,为了提高姿态角跟踪精度,构造了一种新的有限时间扰动观测器。研究结果-对涉及干扰的再入飞行器进行了模拟。结果表明,该方法具有有限时间收敛性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Observer-based finite-time sliding mode control for reentry vehicle
Purpose – The purpose of this paper is to design a disturbance observer-based finite-time global sliding mode control scheme for the attitude tracking control problem of the reentry vehicle with parameter uncertainties and disturbances. Design/methodology/approach – Feedback linearization is first introduced to transform vehicle model into three independent second order uncertain subsystems. Then a finite-time controller (FTC) is proposed for the nominal system on the basis of the homogeneity theory. Thereafter the integral sliding mode method is introduced for the vehicle with disturbances. The finite time convergence is achieved and global robustness is also assured by the combination of finite time control method and integral sliding mode strategy. Furthermore, to improve the attitude angle tracking accuracy a novel finite time disturbance observer (DO) is constructed. Findings – Simulation is made for the reentry vehicle with disturbances involved. And the results show the finite-time convergence, tra...
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来源期刊
CiteScore
6.80
自引率
4.70%
发文量
26
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