引用本文:杨青运,陈谋.考虑输入饱和的近空间飞行器姿态容错控制[J].控制理论与应用,2016,33(11):1449~1456.[点击复制]
YANG Qing-yun,CHEN Mou.Fault-tolerant attitude control for near space vehicles with input saturation[J].Control Theory and Technology,2016,33(11):1449~1456.[点击复制]
考虑输入饱和的近空间飞行器姿态容错控制
Fault-tolerant attitude control for near space vehicles with input saturation
摘要点击 3588  全文点击 1355  投稿时间:2016-03-31  修订日期:2016-07-10
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DOI编号  10.7641/CTA.2016.60177
  2016,33(11):1449-1456
中文关键词  近空间飞行器  干扰观测器  输入饱和  容错控制
英文关键词  near space vehicles  disturbance observer  input saturation  fault-tolerant control
基金项目  国家自然科学基金(61573184, 61374212), 江苏省自然科学基金(SBK20130033), 教育部博士点基金(20133218110013), 江苏省六大高峰人才项目 (2012–XXRJ–010)
作者单位E-mail
杨青运 南京航空航天大学 yang_980060@163.com 
陈谋* 南京航空航天大学 chenmou@nuaa.edu.cn 
中文摘要
      针对近空间飞行器姿态控制中出现的执行器故障, 输入饱和与外部干扰等问题, 设计了一种基于二阶滑模 干扰观测器和辅助系统的鲁棒容错跟踪控制方法. 首先, 将系统不确定, 外部扰动和执行器故障作为复合干扰, 设 计super-twisting二阶滑模干扰观测器对其进行估计. 然后为解决输入饱和问题构造了辅助分析系统, 并借助 backstepping方法, 设计姿态容错跟踪控制器. 利用Lyapunov方法, 严格证明了所有闭环系统信号的收敛性. 最后将 所设计的控制方法应用于近空间飞行器姿态控制中, 仿真结果验证了该控制方法的有效性.
英文摘要
      In this paper, a robust fault-tolerant attitude control scheme is investigated for the near space vehicles (NSVs) with actuator faults, input saturation and unknown external disturbances. Firstly, a super-twisting second order sliding mode disturbance observer is developed to estimate the unknown compound disturbances including system uncertainties, external disturbances and actuator faults. Then, based on the backstepping technology and an auxiliary system constructed to solve the input saturation problem, a attitude fault-tolerant controller is proposed. In addition, the convergence of all the closed-loop system signals under the designed controller is rigorously proved using Lyapunov method. Finally, the proposed control scheme is applied to the attitude control of the NSV, and the effectiveness of this proposed control scheme is demonstrated by the simulation results.