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非线性不确定性系统的变结构控制策略研究 被引量:4

Research on a New Variable Structure Control Law for Non-Linear Plants with Uncertainties
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摘要 针对具有匹配和失配不确定性因素的非线性单变量时变系统,研究了一种新的变结构控制律的设计方法,提出了完全基于对象标称模型和不确定性因素上下界的逻辑极值控制律形式,以保证变结构控制系统渐近稳定或最终有界。 In this paper, a new variable structure control law that is called logic and extreme control law is proposed for nonlinear single--input time-variant plants with matched or mismatched uncertainties. Its design method, which is totally based on the plant ideal model andthe uncertaintiesl extreme values, is also studied' Meanwhile, some direct and general relat.ions between the uncertainties and the control laws' parameters are established. No matterwhat concrete. forms the uncertainties have, the control law designed here ensures that thesliding mode exiSts and the closed loop control system is aspepototically stable or ultimatebounded The results sot in this paper are suited to many areas, such as guided missiles, aircrafts and satellites.
机构地区 西北工业大学
出处 《西北工业大学学报》 EI CAS CSCD 北大核心 1995年第4期614-618,共5页 Journal of Northwestern Polytechnical University
基金 航天科学基金 博士后科学基金
关键词 变结构控制 非线性 控制系统 不确定系统 variable structure control,sliding mode,nonlinear control system,uncertainty
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参考文献1

  • 1高为炳,变结构控制理论基础,1990年

同被引文献23

  • 1刘旭川,申东日,陈义俊.基于输入输出的滑模变结构控制[J].计算机仿真,2005,22(4):67-69. 被引量:5
  • 2胡跃明,刘永清.非匹配条件下滑动模的鲁棒性[J].华南理工大学学报(自然科学版),1995,23(6):36-41. 被引量:2
  • 3刘智平,周凤岐,周军.具有参数不确定性的飞行器的变结构姿态控制[J].宇航学报,2007,28(1):43-48. 被引量:6
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