Classification of actuation mechanism designs with structural block diagrams for flapping-wing drones: A comprehensive review

IF 11.5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Spoorthi Singh , Mohammad Zuber , Mohd Nizar Hamidon , Norkhairunnisa Mazlan , Adi Azriff Basri , Kamarul Arifin Ahmad
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引用次数: 9

Abstract

Flying insects are interesting dipteras with an outstanding wing structure that makes their flight efficient. It is challenging to mimic flying insects and create effective artificial flapping drones that can imitate their flying techniques. The smaller insect-size drones have remarkable applications, but they need lightweight and minimal connecting structures for their transmission mechanism. Many operating methods, such as the traditional rotary actuation method and non-conventional oscillatory mechanisms with multiple transmission configurations, are popularly adopted. The classification and recent design innovations with flapping actuation mechanism challenges, particularly bio-inspired (biomimetics) and bio-morphic types of flapping-wing aerial vehicles from micro to pico-scale, are discussed in this review paper. For ease of understanding, we have attempted to depict the actuation mechanisms in the form of block diagrams. The ability of hybrid efficient mechanisms to improve the flapping frequency of wings and flapping actuation design process, including other parameters, such as flapping angle, lift generation, and hovering ability with current driving mechanisms, is also discussed. Depending on their endearing resemblance, we have segregated Flapping-Wing Micro Air Vehicle (FWMAV) design patterns like birds, small birds, nano hummingbirds, moths, bats, biomorphic types, flapping test bench models, and fully flyable models, which are characterized by their flight modes. Important flapping actuation systems that can be used to achieve hovering capability are highlighted. The actuation mechanisms' specifications and configurations are expanded by focusing on the need of flapping frequency and stroke angle controllability via the linkage mechanisms with insight into flapping patterns. Besides that, the requirements for the sustainability of flying patterns during manual and automatic launches were investigated. In addition, the different researchers' annual progress on their Flapping-wing models has been emphasized. The best performing prototypes with their flapping actuation mechanism contributions to achieving better lift and long-duration flight sustainability are articulated through ranking. An insight into some of the significant challenges and future work on flapping performance levels are also discussed.

扑翼无人机驱动机构结构框图分类设计综述
飞虫是一种有趣的双翅目动物,它们出色的翅膀结构使它们的飞行效率很高。模仿飞行昆虫并制造出能模仿其飞行技术的有效的人工扑翼无人机是一项挑战。更小的昆虫大小的无人机有着非凡的应用,但它们需要轻量级和最小的连接结构作为其传动机构。许多操作方法,如传统的旋转驱动方法和非传统的多传动结构的振荡机构被广泛采用。本文综述了扑翼飞行器的分类和近年来的设计创新与扑翼驱动机制的挑战,特别是从微尺度到微尺度的仿生和仿生扑翼飞行器。为了便于理解,我们试图用方框图的形式来描述驱动机制。讨论了混合高效机构提高机翼扑动频率和扑动设计过程的能力,包括其他参数,如扑动角、升力产生和当前驱动机构的悬停能力。根据它们可爱的相似之处,我们将扑翼微型飞行器(FWMAV)的设计模式分为鸟类、小鸟、纳米蜂鸟、飞蛾、蝙蝠、生物形态类型、扑翼试验台模型和完全可飞模型,这些模型的飞行模式具有其特征。重点介绍了可用于实现悬停能力的重要扑动系统。在了解扑动模式的基础上,重点研究了连杆机构对扑动频率和行程角可控性的需求,扩展了驱动机构的规格和配置。此外,还对手动和自动发射过程中飞行模式的可持续性要求进行了研究。此外,还强调了不同研究人员在扑翼模型方面的年度进展。通过排名阐述了性能最好的原型机及其扑翼驱动机构对获得更好升力和长时间飞行可持续性的贡献。深入了解一些重大的挑战和扑翼性能水平的未来工作也进行了讨论。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Progress in Aerospace Sciences
Progress in Aerospace Sciences 工程技术-工程:宇航
CiteScore
20.20
自引率
3.10%
发文量
41
审稿时长
5 months
期刊介绍: "Progress in Aerospace Sciences" is a prestigious international review journal focusing on research in aerospace sciences and its applications in research organizations, industry, and universities. The journal aims to appeal to a wide range of readers and provide valuable information. The primary content of the journal consists of specially commissioned review articles. These articles serve to collate the latest advancements in the expansive field of aerospace sciences. Unlike other journals, there are no restrictions on the length of papers. Authors are encouraged to furnish specialist readers with a clear and concise summary of recent work, while also providing enough detail for general aerospace readers to stay updated on developments in fields beyond their own expertise.
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