期刊文献+

多自由度微振动环境时域波形复现的数值仿真 被引量:1

Numerical simulation of time domain waveform reproduction of micro-vibration environment of multi-degree of freedom
下载PDF
导出
摘要 为满足航天器微振动环境模拟的需要,开展了多自由度微振动时域波形复现控制方法研究。首先,介绍了基于时域波形复现的多自由度微振动环境模拟控制理论方法。其次,针对六自由度微振动激励系统,应用MATLAB软件建立了基于实测传递函数矩阵的多输入多输出微振动激励仿真系统,针对微振动时域波形复现闭环控制过程进行了算法编程,并给出了仿真的闭环控制流程图。最后,通过算例对多自由度微振动时域波形复现进行了数值仿真,以给定的白噪声为输入,模拟对实际存在的系统非线性、测量误差等影响因素的控制效果。仿真结果验证了多自由度微振动时域波形复现控制方法的可行性及有效性,所得结论可以为研究多自由度微振动时域波形复现控制系统提供参考。 A method of the time domain waveform reproduction (TWR) of micro-vibration of multi-degrees of freedom is proposed to meet the requirement of the micro-vibration environment simulation for spacecraft. Firstly, the theory of the micro-vibration environment simulation based on the time domain waveform reproduction is discussed. Then, a multi-input - multi-output (MIMO) micro-vibration incitation system is established using the MATLAB software based on the transfer function matrix measured in test. The control program for the micro-vibration TWR is developed based on the flow chart of the closed-loop control. Finally, the noise that shows the nonlinear influence of system and measurement errors is added in the simulation examples. Simulation results demonstrate the feasibility and the effectiveness of the control method of the TWR, which could be used for the study of the micro-vibration TWR control of multi-degree of freedom.
出处 《航天器环境工程》 2017年第3期241-246,共6页 Spacecraft Environment Engineering
关键词 微振动环境模拟 多自由度 时域波形复现 控制方法 数值仿真 micro-vibration environment simulation multi-degree of freedom time domain waveform reproduction control method numerical simulation
  • 相关文献

参考文献8

二级参考文献64

  • 1张振华,杨雷,庞世伟.高精度航天器微振动力学环境分析[J].航天器环境工程,2009,26(6):528-534. 被引量:45
  • 2Laskin R A, Sirlin SW. Future Payload Isolation and Pointing System TeChnology[J]. J GuidanCe, 1986, 9(4): 469-477.
  • 3Davis P, Cunningham D, Harrell J. AdvanCed 1.5Hz Passive VisCous Isolation System [C]. AIAA/ASME/ASCE/AHS/ASC StruCtures, StruCtural DynamiCs, and Materials ConferenCe, Hilton Head, USA, April 18-20, 1994.
  • 4Pendergast K J, SChauweCker C J. Use of a Passive ReaCtion Wheel Jitter Isolation System to Meet the AdvanCed X-ray AstrophysiCs FaCility Imaging PerformanCe Requirements [C]. ProCeedings of the 1998 ConferenCe on SpaCe TelesCopes and Instruments V, Kona, USA, MarCh 25-28, 1998.
  • 5Mosier G E, Howard J M, Johnston J D, et al. The Role of Integrated Modeling in the Design and VerifiCation of the James Webb SpaCe TelesCope[C]. SpaCe Systems Engineering and OptiCal Alignment MeChanisms, Denver, USA, August 4-6, 2004.
  • 6NeeCk S P, Venator T J, Bolek J T, Jitter and Stability CalCulation for the ASTER Instrument[C]. Platforms and Systems, Rome, Italy, September 6, 1994.
  • 7MCMiCkell M B, Kreider T, Hansen E, et al. OptiCal Payload Isolation Using the Miniature Vibration Isolation System [C]. Industrial and CommerCial AppliCations of Smart StruCtures TeChnologies, San Diego, USA, MarCh 19-20, 2007.
  • 8Doyle K B. StruCtural Line-of-sight Jitter Analysis for MLCD[C]. New Developments in OptomeChaniCs, San Diego, USA, August 28-30, 2007.
  • 9Ball Corporation. Worldview-2[EB/OL]. [2011]. http ://www. ballaerospaCe, Com/page.jsp?page=82.
  • 10Sannibale V, Ortiz G G, Fan" W H. A Sub-Hertz Vibration Isolation Platform for a Deep SpaCe OptiCal CommuniCation TransCeiver[C]. Free-SpaCe Laser CommuniCation TeChnologies XXI, San Jose, USA, January 28-29, 2009.

共引文献112

同被引文献3

引证文献1

二级引证文献1

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