[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]
导弹与制导技术

降低频带耦合的强静不稳定弹性飞行器控制

  • 王青 ,
  • 张伸 ,
  • 梁津津 ,
  • 董朝阳
展开
  • 1 北京航空航天大学自动化科学与电气工程学院, 北京 100191;
    2 北京航空航天大学航空科学与工程学院, 北京 100191
王青(1968-),女,山东蓬莱人,教授,研究方向:高超声速飞行器制导与控制。

收稿日期: 2017-03-13

  网络出版日期: 2025-05-12

基金资助

国家自然科学基金(61374012)资助

Control of Strongly Stationary Unstable Elastic Spacecraft Which Reduce Coupling of Frequency Band

  • WANG Qing ,
  • ZHANG Shen ,
  • LIANG Jinjin ,
  • DONG Chaoyang
Expand
  • 1 School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China;
    2 School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China

Received date: 2017-03-13

  Online published: 2025-05-12

摘要

针对强静不稳定且刚/弹强耦合的高超声速飞行器,提出了一种新的控制设计方法。首先分析飞行器频带耦合机理,得到刚体对弹性稳定性产生影响的主要因素。继而提出改进双网络控制方法,该方法通过合理设计降低频带耦合,放宽对飞行器静稳定特性的要求,从而能够设计出刚体和弹性性能均满足要求且具有良好鲁棒性和快速性的控制器。将文中所提方案与鲁棒控制方案的结果进行数值仿真对比,验证了该设计方法的优越性。

本文引用格式

王青 , 张伸 , 梁津津 , 董朝阳 . 降低频带耦合的强静不稳定弹性飞行器控制[J]. 弹箭与制导学报, 2017 , 37(6) : 7 -10 . DOI: 10.15892/j.cnki.djzdxb.2017.06.002

Abstract

A new control design method for hypersonic vehicle with strong static instability and rigid/elastic coupling was proposed. Firstly, the frequency band coupling mechanism of aircraft was analyzed to obtain the main factors affecting the elastic stability of rigid body. Then, the improved double-network control method was proposed. Through reducing the coupling of frequency band and relaxing the requirement of static stability characteristics of aircraft, the controller with good robustness and rapidity could be designed to meet the requirements of rigid body and elastic performance. Finally, compared the results of the proposed scheme with the results of robust control scheme, the superiority of the proposed design method was verified.
[an error occurred while processing this directive]

参考文献

[1] SZIROCZAK D, SMITH H. A review of design issues specific to hypersonic flight vehicles[J].Progress in Aerospace Sciences, 2016, 84: 1-28.
[2] 孙长银, 穆朝絮, 余瑶. 近空间高超声速飞行器控制的几个科学问题研究[J].自动化学报, 2013, 39(11): 1901-1913.
[3] 吴宏鑫, 孟斌. 高超声速飞行器控制研究综述[J].力学进展, 2009, 39(6): 756-765.
[4] FIORENTINI L, SERRANI A, BOLENDER M A, et al. Nonlinear robust adaptive control of flexible air-breathing hypersonic vehicles[J].Journal of Guidance, Control, and, Dynamics, 2009, 32(2): 401-416.
[5] ZONG Q, YOU M, ZENG F L. Aeroservoelastic modeling and analysis of six-DOF hypersonic flight vehicle[J].Proceedings of the Institute of Mechanical Engineers. Part G:Journal of Aerospace Engineering, 2016, 230(7): 1240-1251.
[6] MOOIJ E. Numerical investigation of model reference adaptive control for hypersonic aircraft[J].Journal of Guidance, Control, and Dynamics, 2001, 24(2): 315-323.
[7] BUSCHEK H, CALISE A J. Uncertainty modeling and fixed-order controller design for a hypersonic vehicle model[J].Journal of Guidance, Control, and Dynamics, 1997, 20(1): 42-50.
[8] PARKER J T, SERRANI A, YURKOVICH S, et al. Control-oriented modeling of an air-breathing hypersonic vehicle[J].Journal of Guidance, Control, and Dynamics, 2007, 30(3): 856-869.
文章导航

/

[an error occurred while processing this directive]