宇航学报 ›› 2018, Vol. 39 ›› Issue (2): 121-130.doi: 10.3873/j.issn.1000-1328.2018.02.002

• 综述 • 上一篇    下一篇

旋翼式火星无人机技术发展综述

赵鹏越,全齐全,邓宗全,陈水添,杨婷婷   

  1. 哈尔滨工业大学机器人技术与系统国家重点实验室,哈尔滨 150001
  • 收稿日期:2017-07-23 修回日期:2017-11-08 出版日期:2018-02-15 发布日期:2018-02-25
  • 基金资助:

    国家自然科学基金(61403106);高等学校学科创新引智计划(B07018)

Overview of Research on Rotary wing Mars Unmanned Aerial Vehicles

ZHAO Peng yue, QUAN Qi quan, DENG Zong quan, CHEN Shui tian, YANG Ting ting   

  1. State Key Laboratory of Robotics and System, Harbin Institute of Technology, Harbin 150001, China
  • Received:2017-07-23 Revised:2017-11-08 Online:2018-02-15 Published:2018-02-25

摘要:

火星表面稀薄的大气环境为旋翼式无人机在火星低空飞行提供了必要的条件。概述了火星无人机的研究背景、飞行环境与研制难点;整理了世界范围内各研究机构研制的旋翼式火星无人机的技术特点;梳理旋翼式火星无人机研究在气动特性理论、低气压飞行控制、系统集成等方面的关键技术;总结旋翼式火星无人机的仿真研究与实验研究成果;对火星无人机未来的发展趋势进行展望。

关键词: 火星探测, 火星无人机, 旋翼式, 关键技术, 仿真与实验研究

Abstract:

The thin Martian atmosphere provides the necessary condition for Mars unmanned aerial vehicle (UAV) flight. The research background, flight environment and technical difficulties of the Mars UAVs are discussed. Furthermore Mars UAVs developed by different institutes worldwide are summarized. The difficulties of the Mars UAVs in aerodynamic theory, flight control and system integration are combed. The simulation and experimental achievements of the Mars UAVs are also summarized and the development trends of the Mars UAVs are forecasted.

Key words: Mars exploration, Mars UAV, Rotary wing, Key technology, Simulation and experiments

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