Optimal UAV formation guidance laws with timing constraint

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In this paper, optimal guidance laws for multiple vehicles formation flight are addressed. The proposed laws are obtained as state-feedback solutions of linear quadratic optimal control problems to minimize the time varying energy cost with terminal constraints on position and velocity. Since the proposed laws are able to control the flight time, they are possible to make all vehicles join the formation concurrently at a specified time. A method to compensate the acceleration or maneuver of the formation leader is included in the guidance laws. And an inter-vehicle collision avoidance scheme is also considered. The performance of the guidance laws is tested via various numerical simulations.
Publisher
TAYLOR & FRANCIS LTD
Issue Date
2006-05
Language
English
Article Type
Article
Keywords

FORMATION FLIGHT CONTROL; MULTIPLE UAVS

Citation

INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE, v.37, no.6, pp.415 - 427

ISSN
0020-7721
DOI
10.1080/00207720500438340
URI
http://hdl.handle.net/10203/91760
Appears in Collection
AE-Journal Papers(저널논문)
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