Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1718608 | Aerospace Science and Technology | 2011 | 9 Pages |
Abstract
A procedure to compute guidance commands for controlling the relative geometry of multiple unmanned aerial vehicles (UAVs) in formation flight is proposed. The concepts of branch, global leader, and local leader/follower are used to represent the whole formation geometry. A positive-definite function defined in terms of the formation error is then introduced and the Lyapunov stability theorem is used to obtain the cascade type guidance law. This scheme leads to the synchronized flight of all UAVs while maintaining formation geometry. The results of a high fidelity nonlinear simulation of a reconnaissance and surveillance mission example are presented to show the effectiveness of the proposed guidance law.
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Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Tae Soo No, Youdan Kim, Min-Jea Tahk, Gyeong-Eon Jeon,