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Review of the Flight Control Method of a Bird-like Flapping-Wing Air Vehicle.

التفاصيل البيبلوغرافية
العنوان: Review of the Flight Control Method of a Bird-like Flapping-Wing Air Vehicle.
المؤلفون: Fang X; College of Automotive and Mechanical Engineering, Changsha University of Science & Technology, Changsha 410114, China., Wen Y; College of Electrical and Information Engineering, Changsha University of Science & Technology, Changsha 410114, China., Gao Z; College of Automotive and Mechanical Engineering, Changsha University of Science & Technology, Changsha 410114, China., Gao K; College of Automotive and Mechanical Engineering, Changsha University of Science & Technology, Changsha 410114, China.; Hunan Key Laboratory of Smart Roadway and Cooperative Vehicle-Infrastructure Systems, Changsha 410114, China., Luo Q; College of Automotive and Mechanical Engineering, Changsha University of Science & Technology, Changsha 410114, China., Peng H; School of Computer Science and Engineering, Central South University, Changsha 410075, China., Du R; College of Automotive and Mechanical Engineering, Changsha University of Science & Technology, Changsha 410114, China.; Hunan Key Laboratory of Smart Roadway and Cooperative Vehicle-Infrastructure Systems, Changsha 410114, China.
المصدر: Micromachines [Micromachines (Basel)] 2023 Jul 31; Vol. 14 (8). Date of Electronic Publication: 2023 Jul 31.
نوع المنشور: Journal Article; Review
اللغة: English
بيانات الدورية: Publisher: MDPI Country of Publication: Switzerland NLM ID: 101640903 Publication Model: Electronic Cited Medium: Print ISSN: 2072-666X (Print) Linking ISSN: 2072666X NLM ISO Abbreviation: Micromachines (Basel) Subsets: PubMed not MEDLINE
أسماء مطبوعة: Original Publication: Basel, Switzerland : MDPI, [2010]-
مستخلص: The Bird-like Flapping-wing Air Vehicle (BFAV) is a robotic innovation that emulates the flight patterns of birds. In comparison to fixed-wing and rotary-wing air vehicles, the BFAV offers superior attributes such as stealth, enhanced maneuverability, strong adaptability, and low noise, which render the BFAV a promising prospect for numerous applications. Consequently, it represents a crucial direction of research in the field of air vehicles for the foreseeable future. However, the flapping-wing vehicle is a nonlinear and unsteady system, posing significant challenges for BFAV to achieve autonomous flying since it is difficult to analyze and characterize using traditional methods and aerodynamics. Hence, flight control as a major key for flapping-wing air vehicles to achieve autonomous flight garners considerable attention from scholars. This paper presents an exposition of the flight principles of BFAV, followed by a comprehensive analysis of various significant factors that impact bird flight. Subsequently, a review of the existing literature on flight control in BFAV is conducted, and the flight control of BFAV is categorized into three distinct components: position control, trajectory tracking control, and formation control. Additionally, the latest advancements in control algorithms for each component are deliberated and analyzed. Ultimately, a projection on forthcoming directions of research is presented.
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معلومات مُعتمدة: HNJG-2022-0092 Teaching Reform Project for Ordinary Higher Education Institutions in Hunan Province
فهرسة مساهمة: Keywords: flight control; formation control; position control; trajectory tracking control
تواريخ الأحداث: Date Created: 20230826 Latest Revision: 20230829
رمز التحديث: 20240829
مُعرف محوري في PubMed: PMC10456679
DOI: 10.3390/mi14081547
PMID: 37630083
قاعدة البيانات: MEDLINE
الوصف
تدمد:2072-666X
DOI:10.3390/mi14081547