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一类不确定非线性系统的回馈递推滑模鲁棒控制器设计
引用本文:曹邦武,姜长生.一类不确定非线性系统的回馈递推滑模鲁棒控制器设计[J].宇航学报,2005,26(6):818-822.
作者姓名:曹邦武  姜长生
作者单位:1. 南京航空航天大学自动化学院,南京,210016;空军装备部军械通用装备部,北京,100843
2. 南京航空航天大学自动化学院,南京,210016
摘    要:针对一类多输入多输出不确定非线性系统,用一个RBF神经网络获得未建模动态和外来扰动的估计值,将回馈递推思想与滑模控制相结合,逐步回馈递推,设计了鲁捧控制器。将这种方案用于某型侧滑转弯导弹的飞行控制系统设计。其中,为克服导弹作动器的位置饱和、速率饱和问题,改进了滑动面的符号函数,并采用模糊逻辑对滑动面的斜率进行实时调整。仿真表明了该控制方法的有效性。

关 键 词:回馈递推  滑模  模糊控制  神经网络  导弹  飞行控制  作动器饱和
文章编号:1000-1328(2005)06-0818-05
收稿时间:12 23 2004 12:00AM
修稿时间:2004-12-232005-06-28

Robust Backstepping Sliding Mode Controller Design Approach for a Class of Uncertain Nonlinear Systems
CAO Bang-wu,JIANG Chang-shen.Robust Backstepping Sliding Mode Controller Design Approach for a Class of Uncertain Nonlinear Systems[J].Journal of Astronautics,2005,26(6):818-822.
Authors:CAO Bang-wu  JIANG Chang-shen
Abstract:For a class of multiinputmultioutput uncertain nonlinear system,a robust controller based on backstepping and sliding mode control was designed.The unknown dynamics and external disturbances were estimated by a RBF neural network.Then the scheme was applied to design the autopilot system of a skidtoslide missile.Considering the missile's actuator position saturation and velocity saturation,the sign function of the slide mode was improved and fuzzy logic was introduced to adjust the slopes of the sliding mode surfaces.The simulation results show its effectiveness.
Keywords:Backstepping  Sliding mode  Fuzzy control  Neural network  Missile  Autopilot  Actuator saturation
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