期刊文献+

基于模糊逻辑的高速飞行器一体化控制律

An Integrated Control Law for Hypersonic Vehicles Based on Fuzzy Logic
下载PDF
导出
摘要 针对通用高超声速飞行器的非线性模型,提出了一种一体化控制器的设计方法。基于动态逆理论,把非线性模型转换为等价的仿射系统;为等价系统设计模糊逻辑控制器,并基于遗传算法优化模糊逻辑控制参数。仿真表明,该方法能提供满意的鲁棒性、平滑的指令和快速收敛的模糊规则。 An integrated control law is presented by considering a nonlinear model of generic hypersonic vehicle as a plant.Based on dynamic inverse theory,the nonlinear model is transformed into an equivalent affine system.Then a fuzzy logic controller can be designed for the equivalent system.And fuzzy logic control parameters are optimized,which are based on genetic algorithm.The simulation results show that the satisfied robustness,smooth commands and rapid convergence of the fuzzy rules can be supplied by above method.
作者 王健 赵鹏飞
出处 《航天控制》 CSCD 北大核心 2014年第1期44-48,共5页 Aerospace Control
关键词 高超声速 模糊逻辑 动态逆 遗传算法 Hypersonic Fuzzy logic Dynamic inverse Genetic algorithm
  • 相关文献

参考文献6

二级参考文献18

  • 1崔平远.神经网络及其在飞行器建模与控制中的应用[J].飞行力学,1996,14(4):1-7. 被引量:4
  • 2[1]LUKYANOV A G, UTKIN V I. Time-varying linear system decomposed control [C]∥Proc of American Control Conference, Pennsylvania: [s.n.], 1998:2884-2888.
  • 3[2]MAN Z, YU X H. Terminal sliding mode control of MIMO linear systems [J]. IEEE Trans on Circuits and Systems I: Fundamental Theory and Applications, 1997, 44 (11): 1065-1070.
  • 4[3]WU Y, YU X, MAN X. Terminal sliding mode control design for uncertain dynamic systems [J]. Systems & Control Letters, 1998,34(5):281-288.
  • 5[4]YU T. Terminal sliding mode control for rigid robots [J]. Automatica, 1998, 34(1): 51-56.
  • 6[5]FENG Y, YU X, MAN Z. Nonsingular terminal sliding mode control and its applications to robot manipulators [C]∥ Proc of 2001 IEEE Int Symposium on Circuits and Systems, III. Sydney: [s.n.],2001:545-548.
  • 7[6]BHAT S P, BERNSTEIN D S. Finite-time stability of homogeneous systems [C]∥Proc of the American Control Conference. Albuquerque, New Mexico:[s.n.], 1997:2513-2514.
  • 8Wang Q, Stengel R F. Robust nonlinear control of a hypersonic aircraft[A]. AIAA Guidance, Navigation, and Control Conference [C]. Reston, USA: AIAA, 1999. 413-423.
  • 9Marrison C I, Stengel R F. Design of robust control systems for a hypersonic aircraft [ J ]. Journal of Guidance, Control, and Dynamics, 1998, 21 (1) : 58 -63.
  • 10Xu H J, Mirmirani M, Ioannou P A. Robust neural adaptive control of a hypersonic aircraft [ A ]. AIAA Guidance, Navigation,and Control Conference [ C ]. Reston, USA : AIAA, 2003. 1-8.

共引文献19

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