期刊文献+

基于退步控制的再入飞行器自动驾驶仪设计

Backstepping Control Based Autopilot Design for Reentry Aerocraft
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摘要 文中基于一种不同于反馈性化的退步控制思想 ,提出了一种新的非线性反馈自动驾驶仪设计方法 ,利用这种方法 ,为再入飞行器设计了自动驾驶仪。仿真结果表明 ,所提出的退步控制方法是有效的 ,并且设计过程简单 ,易于实现。 In this paper, a new kind of control strategy for design of autopilot with nonlinear feedback based on backstepping technique was presented. Also the autopilot of reentry aerocraft was designed with this nethod. The simulation results show that the method of backstepping proposed in this paper is efficient. The design process is simplex than others and easy for implement.
出处 《弹箭与制导学报》 CSCD 北大核心 2002年第3期14-17,共4页 Journal of Projectiles,Rockets,Missiles and Guidance
关键词 退步控制 再入飞行器 自动驾驶仪 设计 反馈线性化 航天器 reentry aerocraft backsteppong control feedback linearization autopilot
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参考文献5

  • 1Singh S.N.and Stinberg M., Adaptive Control of Feedback Conrol[J]. Jorunal of Guidance, Control and Dynamics July-August 1996,19(4):871-877.
  • 2Jin. Y.C., Chwa D.Y. and Kin. M.S, Adaptive Control for Feedback-Linearized Missiles with Uncertainties[J]. IEEE Trans .on Aerospace and Electronic Systems .Appril 2000,36(2):467-481.
  • 3Schumacher C. and Khargonekar P.Stability Analysis of a Missile Control System with a Dynamic Inversion Controller[J]. Journal of Guidance, Control and Dynamics. May-June ,21(3):508-515.
  • 4Liu X.P., Gu G.X. and Zhou K.Robust stabilization of MIMO nonlinear systems by backstepping[J].Automatica. 1999(35):987-992.
  • 5Ferrara A. and Giacomini L.On modular backstepping design with second order sliding modes[J]. Automatica. 2001(37):129-135.

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