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具有频域指标约束的BTT导弹自动驾驶仪二次型法设计 被引量:8

A BANK-TO-TURN MISSILE AUTOPILOT DESIGN APPROACH USING LQR CONTROL THEORY WITH FREQUENCY DOMAIN CONSTRAINT CONDITIONS
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摘要 本文研究了线性二次型最优控制系统的加权阵与频域指标间的对应关系,基于回路成形理论给出了加权阵选择方法,并将其应用于BTT导弹的自动驾驶仪设计。在建立了无静差控制模型的基础上,获得了满足预定频域指标的设计结果,并通过自动驾驶仪系统的非线性仿真验证了设计方法的有效性。 In this paper, we discussed a correlation of the frequency domain performance and the weighting matrices for linear quadratic optimal control system. Based on the loop shaping theory, a method determining weighting matrices is given, and it is used to design a bank-to-turn (BTT) missile autopilot. Based on the zero steady state error control model,design results to satisfy frequency domain performance requirements are obtained,and the effectiveness of this method is verified by nonlinear simulation of a certain autopilot system.
机构地区 哈尔滨工业大学
出处 《宇航学报》 EI CSCD 北大核心 1995年第2期6-12,共7页 Journal of Astronautics
基金 国家自然科学基金
关键词 倾斜转弯导弹 自动驾驶仪 调节器 BTT missile Autopilot Optimal regulator
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  • 1郑建华,栾泽威,崔平远,杨涤.BTT导弹自动驾驶仪多变量频域设计方法[J].宇航学报,1994,15(3):24-29. 被引量:6
  • 2钱杏芳 张鸿端 等.导弹飞行力学[M].北京:北京工业学院出版社,1987..
  • 3Mustafa Denis, Glover Keith. Controller reduction by H∞ balanced truncation [ C ] // IEEE Trans. on automatic control, 1991.
  • 4Mracek Curtis P, Brett Ridgely D. Missile longitudinal autopilots: connections between optimal control and classical topologies[ C] // AIAA , 2005.
  • 5Skogestad Sigurd, Postlethwaite Ian. Multivariable feedback control-analysis and design[M]. Chichester & John Wiley Sons Ltd, 1996:40-62.
  • 6[1]Ryu J H,Tahk M J.Plant Inversion Control of Tail-Controlled Missiles[A].Proceedings of the AIAA Guidance,Navigation,and Control Conference[C]. New Orleans,Louisiana,1997.
  • 7[2]Bartolini G,Pisano A,Usai E.Global Stabilization of Nonlinear Uncertan Systems with Unmodelled Actuator Dynamics[J].IEEE Transactions on Automatic Control,2001,46(11):1 826-1 832.
  • 8[3]Bartolini G.Chattering Avoidance by Second-order Sliding Mode Control[J].IEEE Transactions on Automatic Control,1998,43(2):1 139-1 141.
  • 9Devaud E, Harcaut J P, Siguerdidjane H. Three-axes missile autopilot design: from linear to nonlinear control strategies[J]. Guid Contr Dyn,2001, 24 (1) :64-71.
  • 10Isidori A. Nonlinear control systems[M]. Third Edition, Springer-Verlag, 1995. 164.

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