基于指令滤波反步法的再入飞行器姿态控制
Attitude Control for a Generic Reentry Vehicle via Command Filtered Back-Stepping Technology
DOI: 10.12677/DSC.2017.61003, PDF, HTML, XML,  被引量 下载: 1,827  浏览: 4,471  国家自然科学基金支持
作者: 吉月辉：天津市复杂系统控制理论及应用重点实验室&天津理工大学自动化学院，天津；周海亮：天津市计量监督检测科学研究院，天津
关键词: 再入飞行器；指令滤波反步法；姿态控制；Reentry Vehicle； Command Filtered Back-Stepping Technology； Attitude Control
摘要: 针对再入飞行器，提出一类新型的简洁的指令滤波反步法，设计动态的状态反馈姿态控制器。所设计的指令滤波反步控制器中，构建积分滑模滤波器逼近虚拟控制输入及其导数，避免传统反步法中复杂的解析推导过程，解决传统反步法中“计算爆炸”问题。在闭环系统中，采用输入状态稳定性和非线性小增益定理分析并保证闭环系统的稳定性和状态信号的有界性。最后，在仿真中验证了所提出姿态控制方法的有效性。
Abstract: A command filtered back-stepping technology is exploited and analyzed to design a dynamic state- feedback attitude controller for a generic reentry vehicle in the technical notes. In the underlying command filtered back-stepping controller, sliding-mode-based integral filters are introduced to estimate the virtual control terms and their derivatives, obviating the complex analytical compu-tation process, subsequently solving the problem of “explosion of computation” in traditional back-stepping approach. The stability analysis of the closed-loop system and the convergence of the aerodynamic angles are verified based on the input-to-state stability and small-gain theorem. Numerical simulations are included to demonstrate the effectiveness of the proposed control scheme.
文章引用：吉月辉, 周海亮. 基于指令滤波反步法的再入飞行器姿态控制[J]. 动力系统与控制, 2017, 6(1): 16-27. http://dx.doi.org/10.12677/DSC.2017.61003

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