基于代理模型探索大黄蜂启发的火星悬停动力优化扑翼设计

Q4 Engineering
Tianyang Xiao, Hao Liu
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引用次数: 5

摘要

虽然漫游车在各种监视方面对火星探测至关重要,但由于火星上地形崎岖和复杂的湍流环境,表面漫游车可能会遇到巨大挑战,部分原因是由于大气密度极低,飞行器难以在空中飞行。火星表面漫游者的飞行在低雷诺数流态方面与地球上的昆虫飞行具有空气动力学相似性。由于昆虫在高度不稳定的环境下可以在产力、飞行稳定性和机动性方面取得显著的扑翼空气动力学性能,我们在这里提出了一种以大黄蜂为灵感的火星表面探测车扑翼设计。我们通过将替代模型和仿生动态飞行模拟器相结合,开发了一个功率高效的空气动力学模型,用于在包括机翼形状和机翼运动学的参数空间中悬停飞行,以探索可行的设计点和一些功率输出最小化的最优解。我们的研究结果表明,受大黄蜂启发的放大机翼模型能够通过一组纵横比和机翼运动学在火星上维持悬停飞行,并找到了与0.0509W的功率输出相对应的最佳设计点,这可能为火星上的扑翼飞行器提供一种新颖可行的仿生设计。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Exploring a bumblebee-inspired power-optimal flapping-wing design for hovering on Mars based on a surrogate model
While rovers are of importance for Mars exploration in terms of various surveillance, surface rovers may encounter great challenges due to rough terrain and complex turbulent environment on Mars partly because aerial vehicles have difficulties to stay airborne due to the extremely low atmospheric density. Flights of surface rovers on Mars share the aerodynamic similarity with insect flights on earth in terms of low Reynolds number flow regime. Motivated by that insects can achieve remarkable flapping-wing aerodynamic performance in force production, flight stability and maneuverability under highly unsteady environments, we here proposed a bumblebee-inspired flapping-wing design for Mars surface rovers. We developed a power-efficient aerodynamic model by combining a surrogate model and a bioinspired dynamic flight simulator for hovering flight in a parametric space comprising wing shape and wing kinematics to explore feasible design points and some optimal solution with the power output minimized. Our results indicate that an enlarged wing model inspired by bumblebees is capable of sustaining hovering flight on Mars with a set of aspect ratios and wing kinematics and an optimal design point is found to correspond with a power output of 0.0509W, which may provide a novel and feasible biomimetic design for flapping-wing aerial vehicles on Mars.
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来源期刊
Journal of Biomechanical Science and Engineering
Journal of Biomechanical Science and Engineering Engineering-Biomedical Engineering
CiteScore
0.90
自引率
0.00%
发文量
18
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