基于自适应近似变结构理论的KKV复合控制系统设计

Liu Hao, Shen Yi
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引用次数: 3

摘要

提出了一种基于自适应逼近变结构控制(AAVSC)理论的高机动动力杀伤飞行器(KKV)鲁棒控制器设计方法,该方法采用气动尾翼和直接力相结合的方式控制姿态。利用这种方法,可以基本解决由于无限频率开关函数的存在而引起的聊天问题。此外,利用在线辨识技术可以很容易地获得确定性结构已知的不确定性和扰动的边界,从而使复合控制系统保持稳定。理论分析和数值仿真结果表明,自适应逼近变结构控制律对参数扰动和干扰具有较强的鲁棒性。由于直接力的作用,响应时间可大大缩短;因此,可以满足KKV的快速响应要求。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Compound control systems design for KKV based on the theory of adaptive approximate variable structure
A robust controller design method for high-maneuverable kinetic kill vehicle (KKV) whose attitude is controlled by combining aerodynamic tail fins and direct force is presented in this paper, which is a new algorithm based on adaptive approximation variable structure control (AAVSC) theory. Using this approach chatting problem which is due to the presence of infinite frequency switching function can be solved basically. In addition, the boundaries of uncertainties and disturbances, whose deterministic structures are known exactly, can be obtained easily by using the technology of the on-line identification, which will make the compound control systems remain stable. Theoretical analysis and numerical simulation results show that adaptive approximation variable structure control law is robust against parameter perturbations and disturbances. Due to the effect of direct force, the response time can be dramatically shortened; therefore, the rapid response requirements for KKV can be met.
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