用于火星探测的旋翼火星无人机关键技术综述

IF 2.1 Q2 ENGINEERING, MULTIDISCIPLINARY
Pengyue Zhao, Ruihan Li, Peng Wu, Huan Liu, Xifeng Gao, Zongquan Deng
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引用次数: 0

摘要

火星表面稀薄的大气层为火星无人飞行器(UAV)进行低空飞行提供了必要的飞行条件。这项工作全面概述了开发火星无人飞行器的关键技术,特别侧重于旋转翼火星无人飞行器。它总结了全球各研究机构开发的旋转翼火星无人机原型。它回顾了旋转翼火星无人机研究的基本技术,包括火星近地面大气环境、空气动力特性和低压飞行控制原理。作品还总结了旋转翼火星无人机的各种实验装置和地面测试结果。此外,它还讨论了旋转翼火星无人机的未来发展趋势。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Review of Key Technologies of Rotary-Wing Mars UAVs for Mars Exploration
The sparse atmosphere on the surface of Mars provides the necessary flight conditions for Mars unmanned aerial vehicles (UAVs) to perform low-altitude flights. This work presents a comprehensive overview of key technologies in the development of Mars UAVs, with a specific focus on rotary-wing Mars UAVs. It summarizes prototypes of rotary-wing Mars UAVs developed by various global research institutions. It reviews essential technologies in rotary-wing Mars UAV research, including the Mars near-surface atmospheric environment, aerodynamic characteristics, and principles of low-pressure flight control. This work also summarizes various experimental setups and ground test results for rotary-wing Mars UAVs. Furthermore, it discusses the future development trends of rotary-wing Mars UAVs.
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来源期刊
Inventions
Inventions Engineering-Engineering (all)
CiteScore
4.80
自引率
11.80%
发文量
91
审稿时长
12 weeks
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