期刊文献+

快速反射镜传感器故障检测 被引量:2

Sensor Fault Detection of a Fast Steering Mirror
下载PDF
导出
摘要 为提高快速反射镜系统(FSM)的可靠性,本文设计实现了基于观测器的故障检测。首先,建立FSM的动力学模型,得到以状态空间方程表示的FSM系统。接着,基于状态空间方程建立故障检测观测器,通过比较系统传感器测量值和观测器所表示的相应变量信息,生成残差。最后,设计相应的残差评价函数,并将其与阈值函数比较给出传感器故障与否的信息。实验结果表明,在无需额外硬件的条件下,残差向量能够及时正确指示各传感器故障信息。 In order to improve the reliability of a two-axis Fast Steering Mirror(FSM) system with minimum hardware consumption, a fault detection method based on observer was developed. The dynamics model of the two-axis FSM was established firstly, and then the state-space form of the FSM was adopted. An observer for fault detection was designed based on the state-space form. Then the residual vector could be generated by comparing the output of the system with its estimation provided by the observer. Finally, the residual evaluation function was adopted, and a fault can be detected by comparing the residual evaluation function with a threshold. Experimental studies on a prototype system show that the sensor fault signal can be detected by the residual vectors timely and accurately. Meanwhile, the consumption of the hardware and space is decreased.
出处 《光电工程》 CAS CSCD 北大核心 2016年第3期46-51,共6页 Opto-Electronic Engineering
关键词 快速反射镜 观测器 故障检测 fast steering mirror observer fault detection
  • 相关文献

参考文献12

  • 1ZHANG Ruochi, WANG Jianmin, ZHAO Guang, et al. Fiber-based free-space optical coherent receiver with vibration compensation mechanism [J]. Optics Express(S 1094-4087), 2013, 21(15): 18434-18441.
  • 2Ostaszewski M, Vermeer W. Fine steering mirror for the James Webb Space Telescope [J]. Proceeding of SPIE(S0277-786X), 2007, 6665: D6650-D6650.
  • 3Bullard A, Shawki I. Responder (R) Fast Steering Mirror [J]. Proceeding of SPIE(S0277-786X), 2013, 8836: 8836-01-8836-06.
  • 4Pain I, Stobie B, Wright G S, et al. The SPIRE Beam Steering Mirror: a cryogenic 2 axis mechanism for the Herschel Space Observatory [J]. Proceeding ofSPIE(S0277-786X), 2003, 4850: 619-627.
  • 5Gorinevsky D, Hoffmann GM, Shmakova M, et al. Fault tolerance of relative navigation sensing in docking approach of spacecraft [C]//2008 IEEE Aerospace Conference, NewYork, USA, 2008, 1: 2695-2703.
  • 6Blesa J, Rotondo D, Puig V, et al. FDI and FTC of wind turbines using the interval observer approach and virtual actuators/ sensors [J]. ControlEngineering Practice(S0967-0661), 2014, 24: 138-155.
  • 7Gheorghe A, Zolghadri A, Cieslak J, et al. Model-Based Approaches for Fast and Robust Fault Detection in an Aircraft Control Surface Servo Loop From Theory to Flight Tests [J]. IEEE Control Systems Magazine(S1066-033X), 2013, 33(3): 20-26.
  • 8Zolghadri A. Advanced model-based FDIR techniques for aerospace systems: Today chalienges and opportunities [J]. Progress in Aerospace Sciences(S0376-0421), 2012, 53: 18-29.
  • 9XIAO Bing, HU Qinglei, ZHANG Youmin, et al. Fault-Tolerant Tracking Control of Spacecraft with Attitude-Only Measurement Under Actuator Failures [J]. Journal of Guidance Control and Dynamics(S0731-5090), 2014, 37(3): 838-849.
  • 10WANG Tao, XIE Wenfang, ZHANG Youmin. Sliding Mode Reconfigurable Control Using Information on the Control Effectiveness of Actuators [J]. Journal of Aerospace Engineering(S0893-1321), 2014, 27(3): 587-596.

同被引文献26

引证文献2

二级引证文献8

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部