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| 1 | 仿昆虫扑翼微飞行器研究现状与关键技术显示文摘仿昆虫扑翼微飞行器基于对自然界中各类昆虫扑翼飞行机理的仿生,具有尺寸微小、隐蔽性高、灵活机动等优势。依据仿昆虫扑翼微飞行器所普遍采用的静电驱动、压电驱动、电机驱动、电磁驱动和其他驱动等扑翼驱动方式,依次分类介绍并总结目前仿昆虫扑翼微飞行器的发展历程、国内外研究现状和最新进展。同时针对目前仿昆虫扑翼微飞行器所采用的各类驱动方式、飞行方式、控制方案、胸腔机构设计、整机系统共振机制以及机载设备搭载研究等关键技术进行了分析和总结。 | 王晨阳 张卫平 邹阳 | 2018 | 无人系统技术2018，1，4： | 12 |
| 2 | Automated Kinematics Measurement and Aerodynamics of a Bioinspired Flapping Rotary Wing显示文摘 | Jianghao Wu Jian Qiu Yanlai Zhang | 2017 | Journal of Bionic Engineering2017，14，4： | 5 |
| 3 | Design,Fabrication,and Analysis of Flapping and Folding Wing Mechanism for a Robotic Bird显示文摘Emulating periodic main wing movement of a bird for generating lift and thrust remains a significant challenge in developing a robotic bird.The sequences of main wing motion are comprised of flapping,folding,bending,and twisting.In this paper,we concentrate on the flapping and folding motion,and design two wing mechanisms based on a 4-bar linkage structure:one is only for Flapping Motion(FM)and the other is for simultaneous Flapping and Folding Motion(FFM)during a wing stroke.We derive relationships between length and angle of links to analyze kinematic characteristics of the mechanisms and conduct an optimization to select the length parameters of links that allow maximization of the flapping angle.We run a simulation to confirm the performance of the optimized parameters by examining physical properties,and fabricate two wing mechanisms accordingly.In particular,the folding motion is achieved without using an additional actuator.Force measurements to investigate a lift profile of each mechanism and their quantitative comparison of the performance of both types confirm the benefits of the folding motion in the perspectives of wing frequency and lift.We expect that our kinematic formulation,design procedures,and comparative measurement results can help develop a wing mechanism to create a truly biomimetic robotic bird. | Seung Wan Ryu Jong Gu Lee Hyoun Jin Kim | 2020 | Journal of Bionic Engineering2020，17，2： | 4 |
| 4 | 面向扑翼飞行控制的建模与奇异摄动分析显示文摘针对扑翼飞行中的周期性和时标不一现象,以及扑翼飞行实际控制中的问题,本文基于奇异摄动理论,提出了一种针对扑翼周期系统的稳定性分析方法.具体而言,首先建立了扑翼飞行器的多刚体模型,为后文对翅翼动力学的奇异摄动分析铺平道路;其次,对多刚体模型进行简化,抽象出扑翼飞行动力学的核心问题,并针对实际控制中的问题,提出了利用奇异摄动理论分析扑翼飞行周期稳定性的方法,指出了其相对于其他方法的优越性;最后,在自制的四自由度扑翼飞行器完成了真实的飞行实验,验证了所提方法的有效性. | 钱辰 方勇纯 李友朋 | 2022 | 自动化学报2022，48，2： | 3 |
| 5 | 仿生微型扑翼飞行器的研究进展显示文摘随着近几年仿生学和微机电系统(MEMS)的发展,仿生微型扑翼飞行器的研究不断取得新的进展,在军事和民用应用领域具有广泛的应用前景。首先介绍了昆虫类生物扑翼飞行的高升力机理研究,然后回顾了近年来对于仿生微型扑翼飞行器的研究成果,重点介绍了不同驱动方式的仿生微型扑翼飞行器的新型样机,也对仿生微型扑翼飞行器相关的典型微加工技术进行了介绍。最后总结出了当前扑翼飞行器发展面临的问题,并对其未来的发展趋势和应用领域进行了预测与展望。 | 丁美希 赵全亮 马世伟 刘志凯 张萌颖 何广平 | 2023 | 兵器装备工程学报2023，44，3： | 2 |
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