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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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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Abstract 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.
AbstractList 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.
Author Pang, Shengyuan
Tian, Linzhe
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  fullname: Tian, Linzhe
  organization: College of Electronic Information Engineering, Hebei University , China
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CitedBy_id crossref_primary_10_2298_TSCI230115083W
crossref_primary_10_1177_09596518241277971
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Snippet Quadrotor unmanned aerial vehicle (UAV) has become more and more popular due to its high maneuverability, vertical take-off, landing and hovering capability,...
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StartPage 12109
SubjectTerms Control methods
Control stability
Hovering
Maneuverability
Optimal control
Unmanned aerial vehicles
Unmanned helicopters
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Title Control Methods for Quadrotor’s Stability
URI https://iopscience.iop.org/article/10.1088/1742-6596/1948/1/012109
https://www.proquest.com/docview/2546087657
Volume 1948
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