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Experimental investigation on hover performance of a single-rotor system for Mars helicopter

  • Published:2019-03 Issue: Volume:86 Page:582-591
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Zhao Pengyue,Quan Qiquan,Chen Shuitian,Tang Dewei,Deng Zongquan

Funder

National Natural Science Foundation of China

111 Project

International Science and Technology Cooperation Programme

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference44 articles.

1. Design, analysis and performance of a rotary wing MAV;Bohorquez;J. Am. Helicopter Soc.,2001

2. Design of a Martian autonomous rotary-wing vehicle;Datta;J. Aircr.,2015

3. Flight test results for aerially deployed Mars balloons;Jeffery,2007

4. Design of the ARES Mars airplane and mission architecture;Braun;J. Spacecr. Rockets,2006

5. Control of a flapping-wing micro air vehicle: sliding-mode approach;Bluman;J. Guid. Control Dyn.,2018

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1. Numerical Analysis of Low Reynolds Number Compressible Flows with Triangle Airfoil;Advances and Challenges in Advanced Unmanned Aerial Systems;2024

2. Review of Key Technologies of Rotary-Wing Mars UAVs for Mars Exploration;Inventions;2023-11-29

3. Optimization of transonic low-Reynolds number airfoil based on genetic algorithm;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-11-14

4. Aerodynamic Analysis and Deployment Mechanism of A Foldable Mars Quadrotor;2023 IEEE International Conference on Mechatronics and Automation (ICMA);2023-08-06

5. Modeling and experimental study on orientation dynamics of a Mars rotorcraft with swashplate mechanism;Aerospace Science and Technology;2023-07
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