首页 | 本学科首页   官方微博 | 高级检索  
     检索      


Robust formation control for missiles with obstacle avoidance
Authors:Yong GUO  Danvang SONG  Changqing WANG  Jinpeng ZHANG  Gongping ZHANG  Aijun LI
Institution:1. School of Automation, Northwestern Polytechnical University, Xían 710000, China;2. Luoyang Optoelectro Technology Development Center, Luoyang 471000, China;3. Aviation Key Laboratory of Science and Technology on Airborne Guided Weapons, Luoyang 471000, China
Abstract:This paper investigates the robust formation control for missiles with obstacle avoidance.A sliding mode surface that is asymptotically stable is firstly presented by the collision avoidance potential function and hyperbolic tangent function.Based on the sliding mode surface,a robust for-mation controller with obstacle avoidance is designed for missiles.To improve the convergence rate,a finite-time controller which can deal with the formation control for missiles is given using an improved sliding mode surface.Finally,the effectiveness of the designed controllers for missiles is demonstrated by the Lyapunov theory and simulation results.
Keywords:Collision avoidance  Finite-time control  Missile formation  Potential function  Sliding mode control
本文献已被 万方数据 ScienceDirect 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号