中国空间科学技术

中国空间科学技术 ›› 2014, Vol. 34 ›› Issue (5): 10-17.doi: 10.3780/j.issn.1000-758X.2014.05.002

• 研究探讨 • 上一篇    下一篇

基于能耗与可靠性约束的动量轮可重构性评价

 胡宇桑1,2, 王大轶1,2, 刘成瑞1,2   

  1. （1北京控制工程研究所，北京100190）（2空间智能控制技术重点实验室，北京100190）
  • 收稿日期:2014-03-06 修回日期:2014-04-24 出版日期:2014-10-25 发布日期:2014-10-25
  • 作者简介:胡宇桑 1989年生，2014年获北京控制工程研究所控制科学与工程专业硕士学位，助理工程师。研究方向为导航、制导与控制。
  • 基金资助:

    国家自然科学基金(61203093,61004073)资助项目

ReconfigurabilityEvaluationofMomentumWheelControlSystemUnderEnergyandReliabilityConstraints

 HU  Yu-Sang1,2, WANG  Da-Yi1,2, LIU  Cheng-Rui1,2   

  1. （1BeijingInstituteofControlEngineering,Beijing100190）
    （2ScienceandTechnologyonSpaceIntelligentControlLaboratory,Beijing100190）
  • Received:2014-03-06 Revised:2014-04-24 Published:2014-10-25 Online:2014-10-25

PDF (PC)

1324

被引次数

3

摘要： 针对目前在控制系统的可重构性评价中较少考虑系统能耗、可靠性限制的问题，文章研究了约束条件下卫星姿态控制系统可重构性度量及评价方法，建立了含执行机构失效因子的控制系统模型，并基于可控性格兰姆矩阵得到能耗约束下可重构性度量指标；然后将可靠性指标引入到系统可重构性评价度量中，进一步缩小可重构性集合；最终形成综合两种约束的可重构性评价方法。通过对含动量轮系统的重构构型仿真，得到约束前后的可重构性对比，仿真结果符合实际分析，验证了该方法的有效性。

关键词: 可重构性, 可靠性, 执行机构失效, 容错控制, 故障诊断, 卫星

Abstract: Since the energy consumption and system reliability constraint was rarely considered in the control system reconfigurability evaluation, the reconfigurability measurement and evaluation method were studied under the constraints for the satellite attitude control system. The control system model including the actuator failure factor was established. Based on the controllability Gramian Matrix, the reconfigurability measurement index under energy consumption was obtained. Furthermore, the control reconfigurability index was introduced into the system reliability constraint, which narrowed the set of reconfigurable systems. Finally, the combined index was obtained. From the control system with momentum wheels simulation, the reconfigurability comparison results among different constraints can be acquired. The results show that this evaluation method is effective.

Key words: Reconfigurability, Reliability, Fault-tolerantcontrol, Actuatorfailure, Faultdiagnosis, Satellite