Control Methods for Quadrotor’s Stability

Quadrotor unmanned aerial vehicle (UAV) has become more and more popular due to its high maneuverability, vertical take-off, landing and hovering capability, and ease of operation. However, it is subject to various disturbances during the flight, such as turbulence. This paper provides a comprehensi...

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Bibliographic Details
Published inJournal of physics. Conference series Vol. 1948; no. 1; pp. 12109 - 12123
Main Authors Pang, Shengyuan, Tian, Linzhe
Format Journal Article
LanguageEnglish
Published Bristol IOP Publishing 01.06.2021
Subjects
Control methods
Control stability
Hovering
Maneuverability
Optimal control
Unmanned aerial vehicles
Unmanned helicopters
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Summary:Quadrotor unmanned aerial vehicle (UAV) has become more and more popular due to its high maneuverability, vertical take-off, landing and hovering capability, and ease of operation. However, it is subject to various disturbances during the flight, such as turbulence. This paper provides a comprehensive survey of control methods proposed for quadrotor stability. According to the relationship between the controller and the controlled model, this paper divides the quadrotor stability control methods into three categories, namely classical control, optimal control, and intelligent control, for detailed discussion.
Bibliography:ObjectType-Article-1
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ISSN:1742-6588
1742-6596
DOI:10.1088/1742-6596/1948/1/012109