DocumentCode
574464
Title
Formation flight of unmanned rotorcraft based on robust and perfect tracking approach
Author
Biao Wang ; Xiangxu Dong ; Chen, Ben M. ; Lee, Tong H. ; Swee King Phang
Author_Institution
Dept. of Electr. & Comput. Eng., Nat. Univ. of Singapore, Singapore, Singapore
fYear
2012
fDate
27-29 June 2012
Firstpage
3284
Lastpage
3290
Abstract
The paper presents a control scheme to the formation flight of a pair of unmanned rotorcraft. A leader-follower formation strategy is adopted and it is realized by utilizing the robust and perfect tracking (RPT) control approach. More specifically, individual RPT flight control laws are implemented in each aircraft, while the measurements from its neighbor and its own sensors are both taken into account for feedback to each aircraft system. In addition, a formation command generator is executed on the follower to ensure that it remains in formation with the leader. This control scheme facilitates the construction of formation flight systems and eases the changing of formation scale. Finally, the proposed formation flight strategy is realized and its performance is verified through several flight tests.
Keywords
aerospace testing; autonomous aerial vehicles; helicopters; multi-robot systems; position control; tracking; RPT flight control law; aircraft system; feedback; flight testing; formation command generator; formation flight system; leader-follower formation strategy; perfect tracking control approach; robust tracking control approach; sensor; unmanned rotorcraft; Acceleration; Equations; Helicopters; Lead; Mathematical model; Robustness;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference (ACC), 2012
Conference_Location
Montreal, QC
ISSN
0743-1619
Print_ISBN
978-1-4577-1095-7
Electronic_ISBN
0743-1619
Type
conf
DOI
10.1109/ACC.2012.6315049
Filename
6315049
Link To Document