期刊文献+

一种改进的自适应模糊滑模大包线飞行控制方法 被引量:3

Improved Adaptive Fuzzy Sliding Mode Large Envelope Flight Control Method
下载PDF
导出
摘要 提出了一种改进的自适应模糊滑模大包线飞行控制方法。该方法以经模拟退火粒子群算法优化的小波神经网络实现非线性模型的逆,能够更加细致地逼近非线性模型,并针对自适应控制的鲁棒性与瞬态性能差的缺点,将滑模控制与自适应控制相结合共同补偿逆误差,提高了自适应控制的鲁棒性与瞬态性。仿真结果表明:所设计的自适应模糊滑模大包线飞行控制器具有优良的控制性能。 An improved adaptive fuzzy sliding mode large envelope flight control method was approved. The method realized the inversion of the nonlinear model using wavelet neural network. In order to approach the nonlinear model accurately, the wavelet neural network was optimized using simulated annealing particle swarm optimization algorithm. The sliding mode control was used to compensate the inversion error with adaptive control for improving robustness and transient characteristic performance. The simulation results show the design adaptive fuzzy sliding mode large envelope flight controller has excellent control performance.
出处 《系统仿真学报》 EI CAS CSCD 北大核心 2008年第5期1262-1264,1278,共4页 Journal of System Simulation
关键词 非线性控制 自适应控制 小波神经网络 滑模控制 模拟退火 nonlinear control adaptive control wavelet neural network sliding mode control simulated annealing
  • 相关文献

参考文献7

  • 1Kim B S, Calise A J. Nonlinear flight control using neural networks [J]. AIAA Journal of Guidance, Control and Dynamics (S0731-5090), 1997, 20(1): 26-33.
  • 2周国栋,胡延霖,于克振.一种新的神经网络自适应逆飞行控制[J].航空兵器,2006,13(4):3-6. 被引量:4
  • 3Wan E A, Bogdanov A A. Model predictive neural control with applications to a 6 DOF helicopter model [C]// Proceedings of American Control Conference. Arlington: IEEE, 2001: 488-93.
  • 4Ciann-Dong Yang, Chien-Chung Kung. Nonlinear flight control of general six-degree-of-freedom Motions [J]. Journal of Guidance, Control, and Dynamics (S0731-5090), 2000, 23(2): 278-288.
  • 5Isidoria. Nonlinear Control Systems [M]. Berlin: Springer, 1995.
  • 6Wisek B J. Stability and flying quality robustness of a dynamic inversion aircraft control law [J]. J. of Guidance, Control and Dynamics (S0731-5090), 1996, 19(6): 1270-1278.
  • 7Shi Y, Eberhart R. Fuzzy adaptive particle swarm optimization [C]// IEEE World Congress on Evolutionary Computation. Seoul: IEEE, 200h 101-106.

二级参考文献1

共引文献3

同被引文献29

  • 1李正强,张怡哲,宋述杰,邓建华.非线性结构自适应模型逆飞行控制律设计研究[J].西北工业大学学报,2009,27(4):471-476. 被引量:2
  • 2陈谋,姜长生,吴庆宪.基于多模型方法的全包络鲁棒飞行控制器设计[J].航空学报,2006,27(3):486-492. 被引量:15
  • 3余翔,李俨,王新民,沈宁.基于LMI的直升机线性二次型可靠控制律设计[J].系统仿真学报,2007,19(15):3521-3523. 被引量:1
  • 4Aeronautical Design Standard: Handling Qualities Requirements for Military Rotorcraft (ADS-33D) [S]. U. S. Army Aviation and Troop Command, Directorate for Engineering, July, 1994.
  • 5Jonas Witt, Sudchai Boonto, Herbert Werner. Approximate model predictive control of a 3-DOF helicopter[C]//46^th IEEE Conference on Decision an Control, New Orleans, LA, USA, Dec, 2007. USA: IEEE, 2007: 4501-4506.
  • 6Jiyang Dai, Jiangqm Mao, Weiqiang Wan, Yanxia Li, Er Meng Joo.. Fuzzy switching control law design for helicopters. TENCON '02. Proceedings [C]//2002 IEEE Region 10^th Conference on Computers, Communications, Control and Power Engineering. USA: IEEE, Oct. 2002: 1634-1637.
  • 7Hedrick J K, Gopalswamy S.Nonlinear flight control design via sliding methods[J].Joumal of Guidance, Control and Dynamics, 1990,13(5): 850-858.
  • 8Adams R J, Banda S S.Robust flight control design using dynamic inversion and structured singular value synthesis[J].IEEE Transactions on Control Systems Technology, 1993,1 (2) : 80-92.
  • 9Yang C D, Kung C C.Nonlinear H∞ flight control of general six-degree-of-freedom motions[J].Journal of Guidance, Control and Dynamics,2000,23(2) :278-288.
  • 10Wang Q, Stcngcl R F.Robust nonlinear flight control of a high-performance aircraft[J].IEEE Transactions on Control Systems Technology, 2005,13 (1) : 15-26.

引证文献3

二级引证文献13

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