Flight Control System of Unmanned Aerial Vehicle

被引：19
作者：
浦黄忠 [1 ]
甄子洋 [2 ]
夏曼 [2 ]
机构：
[1] UAV Research Institute,Nanjing University of Aeronautics and Astronautics
[2] College of Automation Engineering,Nanjing University of Aeronautics and Astronautics
来源：
TransactionsofNanjingUniversityofAeronauticsandAstronautics | 2015年 / 32卷 / 01期
基金：
中国国家自然科学基金; 中央高校基本科研业务费专项资金资助;
关键词：
unmanned aerial vehicle(UAV); flight control; optimal control; adaptive control; intelligent control;
D O I：
10.16356/j.1005-1120.2015.01.001
中图分类号：
V249.1 [飞行控制]; V279 [无人驾驶飞机];
学科分类号：
081105 ; 1111 ;
摘要：
To date unmanned aerial system(UAS)technologies have attracted more and more attention from countries in the world.Unmanned aerial vehicles(UAVs)play an important role in reconnaissance,surveillance,and target tracking within military and civil fields.Here one briefly introduces the development of UAVs,and reviews its various subsystems including autopilot,ground station,mission planning and management subsystem,navigation system and so on.Furthermore,an overview is provided for advanced design methods of UAVs control system,including the linear feedback control,adaptive and nonlinear control,and intelligent control techniques.Finally,the future of UAVs flight control techniques is forecasted.
引用
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页码：1 / 8
页数：8
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