Novel decoupling-compensating control based on incremental model for bank-to-turn missiles
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摘要: 详细分析了倾斜转弯(BTT, Bank-To-Turn)导弹传统动态逆控制的特点及其存在的问题,在此基础上提出了一种基于增量模型的BTT导弹解耦补偿控制方法.该方法通过建立一种描述从当前动态转移至期望动态的BTT导弹增量模型,消除了难以测量或不确定较大的模型部分;在此基础上结合动态逆控制思想设计了BTT导弹的增量式解耦跟踪控制律,与传统动态逆相比,该控制律对模型的依赖程度大幅降低;为进一步提高控制系统对干扰的适应性,提出了一种简单的干扰估计/补偿策略;最后通过数学仿真验证了该方法的有效性.Abstract: The characteristic and existed problems of traditional dynamic inversion control for bank-to-turn (BTT) missiles were analyzed in detail. A novel decoupling-compensating control approach was proposed for BTT missiles. In this approach, an incremental BTT model which demonstrated the transition from current dynamics to desired dynamics was established. And by doing so, the portion of model which was difficult to observe or with large uncertainties was eliminated. Then based on the incremental model and dynamic inversion, the incremental decoupling-tracking control law was designed which relied less on model than the traditional dynamic inversion. To further improve the control law’s adaptability to disturbances, a simple disturbance estimation and compensation strategy was proposed. Finally, simulation results validate the effectiveness of this approach.
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Key words:
- bank-to-turn missiles /
- dynamic inversion /
- incremental model /
- nonlinear control /
- adaptive control
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[1] Arrow A.An analysis of aerodynamic requirements for coordinated bank-to-turn autopilots .NASA-CR-3644,1982 [2] Kim J,Jang J.Nonlinear model inversion control for bank-to-turn missile .AIAA-1995-3318,1995 [3] Wee L B.Nonlinear autopilot design for bank-to-turn steering of a flight vehicle[J].Journal of Guidance Control and Dynamics,1996,19(4):978-979 [4] 张艳,段朝阳,张平,等.基于动态逆的BTT导弹自动驾驶仪设计[J].北京航空航天大学学报,2007,33(4):422-426 Zhang Yan,Duan Chaoyang,Zhang Ping,et al.BTT missile autopilot design based on dynamic inversion[J].Journal of Beijing University of Aeronautics and Astronautics,2007,33(4):422-426(in Chinese) [5] 于秀萍.基于动态逆系统和神经网络理论的BTT导弹控制系统研究 .哈尔滨:哈尔滨工程大学自动化学院,2004 Yu Xiuping.The research of BTT missile control system based on dynamic inversion system and neural network theory .Harbin:College of Automation,Harbin Engineering University,2004(in Chinese) [6] Cho D,Kang S,Kim H.Adaptive dynamic surface control based on neural network for missile autopilot .AIAA-2011-6251,2011 [7] 曾宪法,王洁瑶,王小虎,等.基于SMDO的滑模控制器设计及其在导弹上的应用[J].航空学报,2011,32(5):873-880 Zeng Xianfa,Wang Jieyao,Wang Xiaohu,et al.Design of sliding mode controller based on SMDO and its application to missile control[J].Acta Aeronautics et Astronautica Sinica,2011,32(5):873-880(in Chinese) [8] Ahn C,Kim Y,Kim H.Adaptive sliding mode control for non-affine nonlinear vehicle systems .AIAA-2007-6506,2007 [9] Aaron J O,Barton J B.Enhanced NDI strategies for reconfigurable flight control //Proceedings of the American Control Conference.Anchorage:IEEE,2002:3631-3636 [10] 郑建华,杨涤.鲁棒控制理论在倾斜转弯导弹中的应用[M].北京:国防工业出版社,2001:86-88 Zheng Jianhua,Yang Di.The application of robust control theory to bank-to-turn missile[M].Beijing:National Defense Industry Press,2001:86-88(in Chinese) [11] 彭冠一.防空导弹武器制导控制系统设计[M].北京:中国宇航出版社,1996:381-385 Peng Guanyi.Air Defense missile weapons’ guidance and control system design[M].Beijing:China Astronautic Press,1996:381-385(in Chinese) [12] 韩京清,王伟.非线性跟踪-微分器[J].系统科学与数学,1994,14(2):177-183 Han Jingqing,Wang Wei.Nonlinear tracking-differentiator[J].Journal of System Science & Mathematical Sciences,1994,14(2):177-183(in Chinese)
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