DocumentCode
3371405
Title
Multi-Unmanned Helicopter formation control on relative dynamics
Author
Zheng Wang ; He, Yuqing ; Han, Jianda
Author_Institution
Grad. Sch. of Chinese Acad. of Sci., Chinese Acad. of Sci., Shenyang, China
fYear
2009
fDate
9-12 Aug. 2009
Firstpage
4381
Lastpage
4386
Abstract
Multiple Unmanned Helicopters (UH) formation control is a difficult problem due to the highly nonlinear model and extensively existing uncertainties. In this paper, basing on the concept of relative dynamics and Leader-Follower formation strategy, a new formation control algorithm is given to partially solve this problem. First, the formation control problem is transformed into tracking problems of multiple Leader-Follower partners, and the relative dynamics model is derived by combining a fully dynamics model of follower UH system and a simplified model of leader UH system. Second, with the approximate feedback linearization method, a nonlinear robust tracking controller is designed by the H¿ control technology. Finally, simulations of the new proposed method with two UH systems are conducted, and the results are compared with the normal Leader-Follower formation control algorithm to show the improvement.
Keywords
H¿ control; aircraft control; feedback; mobile robots; multi-robot systems; nonlinear systems; remotely operated vehicles; robot dynamics; robust control; H¿ control technology; UH system; feedback linearization method; leader follower formation strategy; multiunmanned helicopter formation control; nonlinear model; nonlinear robust tracking controller; relative dynamics; Aerodynamics; Control systems; Helicopters; Linear approximation; MIMO; Nonlinear control systems; Nonlinear dynamical systems; Robotics and automation; Stability; Vehicle dynamics; Approximate Linearization; Formation Control; H∞ Control; Relative Dynamics; Unmanned Helicopter;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation, 2009. ICMA 2009. International Conference on
Conference_Location
Changchun
Print_ISBN
978-1-4244-2692-8
Electronic_ISBN
978-1-4244-2693-5
Type
conf
DOI
10.1109/ICMA.2009.5246619
Filename
5246619
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