Adaptive Dynamic Surface Control for Integrated Missile Guidance and Autopilot

作     者：Ming-Zhe Hou Guang-Ren Duan 

作者机构：Center for Control Theory and Guidance Technology Harbin Institute of Technology Harbin 150001 PRC 

出 版 物：《International Journal of Automation and computing》 (国际自动化与计算杂志（英文版）)

年 卷 期：2011年第8卷第1期

页      面：122-127页

核心收录：

学科分类：12[管理学] 07[理学] 08[工学] 071102[理学-系统分析与集成] 0711[理学-系统科学] 083002[工学-环境工程] 1204[管理学-公共管理] 0830[工学-环境科学与工程（可授工学、理学、农学学位）] 120402[管理学-社会医学与卫生事业管理(可授管理学、医学学位)] 0837[工学-安全科学与工程] 0802[工学-机械工程] 081101[工学-控制理论与控制工程] 0701[理学-数学] 0811[工学-控制科学与工程] 0812[工学-计算机科学与技术（可授工学、理学学位）] 081103[工学-系统工程] 

基　　金：supported by National Natural Science Foundation of China (No. 60710002  No. 60974044) 

主　　题：Integrated guidance and control unmatched uncertainty adaptive control dynamic surface control homing missiles. 

摘      要：Integrated guidance and control for homing missiles utilizing adaptive dynamic surface control approach is considered based on the three channels independence design idea. A time-varying integrated guidance and control model with unmatched uncertainties is first formulated for the pitch channel, and an adaptive dynamic surface control algorithm is further developed to deal with these unmatched uncertainties. It is proved that the proposed feedback controller can ensure not only the accuracy of target interception, but also the stability of the missile dynamics. Then, the same control approach is further applied to the control design of the yaw and roll channels. The 6-degree-of-freedom （6-DOF） nonlinear missile simulation results demonstrate the feasibility and advantage of the proposed integrated guidance and control design scheme.