DocumentCode
582413
Title
Formation control based on second-order feedback linearization
Author
Lin, Yihui ; Chen, Mou ; Mei, Rong
Author_Institution
Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
fYear
2012
fDate
25-27 July 2012
Firstpage
5014
Lastpage
5018
Abstract
Formation control using feedback linearization is developed in this paper. The purpose of the work is that the relative trajectory between follower and leader is linearized in velocity coordinate system in order to accurately control its dynamic process. Considering not all states of the leader which are necessary for complete linearization can be measured in some cases, both full state feedback and non-full state feedback are discussed for the formation control. When the relative trajectory is affected by the unmeasured states in non-full state feedback case, the bounded position error caused by the disturbance can be guaranteed and the formation controller still works well. Simulation results are presented to demonstrate the formation control performance even if the course angle of the leader is changeable.
Keywords
autonomous aerial vehicles; linearisation techniques; multi-robot systems; position control; state feedback; bounded position error; dynamic process control; formation control; full state feedback; leader course angle; leader-follower structure; multiple UAVs cooperation; multiple unmanned aerial vehicles; nonfull state feedback; relative trajectory; second-order feedback linearization; velocity coordinate system; Aerodynamics; Equations; Lead; Mathematical model; State feedback; Trajectory; Vehicle dynamics; Formation control; dynamic inversion; feedback linearization; helicopter;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2012 31st Chinese
Conference_Location
Hefei
ISSN
1934-1768
Print_ISBN
978-1-4673-2581-3
Type
conf
Filename
6390810
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