典型文献
Robust formation control for missiles with obstacle avoidance
文献摘要：
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.
文献关键词：
中图分类号：
作者姓名：
Yong GUO;Danvang SONG;Changqing WANG;Jinpeng ZHANG;Gongping ZHANG;Aijun LI
作者机构：
School of Automation,Northwestern Polytechnical University,Xi'an 710000,China;Luoyang Optoelectro Technology Development Center,Luoyang 471000,China;Aviation Key Laboratory of Science and Technology on Airborne Guided Weapons,Luoyang 471000,China
文献出处：
引用格式：
[1]Yong GUO;Danvang SONG;Changqing WANG;Jinpeng ZHANG;Gongping ZHANG;Aijun LI-.Robust formation control for missiles with obstacle avoidance)[J].中国航空学报（英文版）,2022(01):70-80
A类：
B类：
Robust,formation,missiles,obstacle,avoidance,This,paper,investigates,robust,sliding,mode,surface,that,asymptotically,stable,firstly,presented,by,collision,potential,function,hyperbolic,tangent,Based,designed,To,convergence,finite,which,can,deal,given,using,improved,Finally,effectiveness,controllers,demonstrated,Lyapunov,theory,simulation,results
AB值：
0.468968
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