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| 基于积分滑模的BTT导弹鲁棒反演控制律设计 | |
| 引用本文： | 董朝阳,陈宇,王青,张燕,张颖昕.基于积分滑模的BTT导弹鲁棒反演控制律设计[J].航空兵器,2011(1):3-8,12. |
| 作者姓名： | 董朝阳 陈宇 王青 张燕 张颖昕 |
| 作者单位： | 1. 北京航空航天大学航空科学与工程学院,北京,100191 2. 北京航空航天大学自动化科学与电气工程学院,北京,100191 3. 中国空空导弹研究院,河南,洛阳,471009 |
| 摘 要： | 针对不确定非线性强耦合BTT导弹的控制器设计问题,将滑模控制与反演控制思想相结合,在标称模型的基础上进行反演控制器设计.针对系统所存在的模型不确定性和外界干扰,增加一个积分滑模补偿器,提高系统的鲁棒性能.该方法通过合理地设计积分滑模面,保证系统初始状态处于滑模面上,消除了滑模到达阶段,从而有效地提高了系统的鲁棒性.仿真... |
| 关 键 词： | 滑模控制 倾斜转弯导弹 积分滑模 鲁棒 反演控制 |
Robust Backstepping Controller Design Based on Integral Sliding Mode Surface for Bank-to-Turn Missiles |
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| DONG Chao-yang,CHEN Yu,WANG Qing,ZHANG Yan,ZHANG Ying-xin.Robust Backstepping Controller Design Based on Integral Sliding Mode Surface for Bank-to-Turn Missiles[J].Aero Weaponry,2011(1):3-8,12. | |
| Authors: | DONG Chao-yang CHEN Yu WANG Qing ZHANG Yan ZHANG Ying-xin |
| Affiliation: | DONG Chao-yang1,CHEN Yu2,WANG Qing2,ZHANG Yan3,ZHANG Ying-xin2(1.School of Aeronautic Science and Engineering,Beijing University of Aeronautics & Astronautics,Beijing 100191,China,2.School of Automation Science and Electrical Engineering,3.China Airborne Missile Academy,Luoyang 471009,China) |
| Abstract: | The sliding mode control and backstepping technology are combined to solve control design problem of bank-to-turn missiles with model uncertainties and strong coupling nonlinear dynamics.First,the backstepping controller is designed based on the nominal model.Then,a compensator based on integral sliding mode surface is used to improve robustness to the model uncertainties and external disturbances.The sliding mode surface is properly designed so that the system can always start at the sliding mode surface.B... |
| Keywords: | sliding mode control bank-to-turn missile integral sliding mode surface robust backstepping control |
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