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