DocumentCode :
1795268
Title :
Distributed control of nonlinear elastic formation of unmanned aerial vehicles
Author :
Xu Guangyan ; Li Zheng
Author_Institution :
Main Studying Direction is Air Dynamics & Control of Spacecraft & its Formation, Shenyang Aerosp. Univ., Shenyang, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
2181
Lastpage :
2186
Abstract :
For an Unmanned Aerial Vehicle (UAV) formation in “leader-follower” mode, a bran-new concept of nonlinear elastic distance vector is proposed, which helps achieve much more excellent control effect. Based on the nonlinear elastic distance vector, through a big mountain of mathematical work the mathematical model of UAV formation flight is built and linearized skillfully. A new model of UAV formation flight is obtained, which has distinct physical meaning and simple form. And on this basis, by introducing some simplification and symmetry of feedback gain, a fire-new high-efficiency distributed controller of elastic formation is designed. Even better, it expends munch small control cost while providing such better control effect. Then the stability of the controller is proved subtly and a very important theorem offers sufficient conditions for the stability of the model is proposed. Simulation results show that controller can keep the formation much more effectively. In addition, the control quantity is only related to two elements: One is the speed of controlled vehicle itself, the other is the relative distance between controlled vehicle and its neighbor. For this reason, the control problem becomes more simple.
Keywords :
autonomous aerial vehicles; control system synthesis; distributed control; feedback; mobile robots; nonlinear control systems; stability; vectors; UAV formation flight mathematical model; distributed control; feedback gain; leader-follower mode; nonlinear elastic distance vector; stability; sufficient conditions; unmanned aerial vehicle nonlinear elastic formation; Acceleration; Aerodynamics; Aerospace control; Educational institutions; Mathematical model; Stability analysis; Vectors; UAV formation; distributed control; nonlinear elastic coefficient;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
Type :
conf
DOI :
10.1109/CGNCC.2014.7007511
Filename :
7007511
Link To Document :
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