Decentralized formation flight via PID and integral sliding mode control

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35
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52

초록

This paper solves a formation control problem for a group of vehicles such as UAVs on a directed network subject to constant and time-varying disturbances or commands. A celebrated PID control is first proposed for constant disturbance rejection. A set of necessary and sufficient conditions for the vehicles to achieve a desired formation is proposed. Then, integral sliding mode control is introduced to tackle unknown but bounded time-varying disturbances or commands. In addition, the control sensitivity with respect to the network topology is analyzed. Finally, a quadcopter formation platform is introduced and used to verify all the presented theoretical results experimentally. (C) 2018 Elsevier Masson SAS. All rights reserved.

키워드

Formation controlTime-varying disturbanceUnmanned aerial vehicle (UAV)Multi-agent systemPID controlIntegral sliding mode controlSPACECRAFT FORMATIONMULTIAGENT SYSTEMSQUADROTORTRACKINGNAVIGATIONDESIGN
제목
Decentralized formation flight via PID and integral sliding mode control
저자
Thien, Rebbecca T. Y.Kim, Yoonsoo
DOI
10.1016/j.ast.2018.08.011
발행일
2018-10
유형
Article
저널명
Aerospace Science and Technology
81
페이지
322 ~ 332