An Unsteady Rotor Aerodynamics Analytical Model of Hybrid Compound High-speed Helicopter-Reference-Cited by-同舟云学术

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An Unsteady Rotor Aerodynamics Analytical Model of Hybrid Compound High-speed Helicopter

Published:2023-11-23 Issue: Volume:5 Page:11-16
ISSN:
Container-title:2023 5th International Conference on Control and Robotics (ICCR)
language:
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Author:

Yin Xinfan¹,Ma Hongxu¹,An Honglei¹,Wei Qing¹,Wang Liangquan²,Nie Bowen¹

Affiliation:

1. College of Intelligence Science and Technology, National University of Defense Technology,Changsha,China

2. Key Laboratory of Rotor Aerodynamics, China Aerodynamics Research and Development Center,Mianyang,China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10444765/10444743/10444885.pdf?arnumber=10444885

Reference15 articles.

1. Development status and key technologies of micro unmanned helicopters;Yin;Aerodynamic Missile Journal,2018

2. Research on modeling and stability control of micro unmanned helicopter

3. Current status, development trend and counter-measure for high-speed rotorcraft;Wu;Journal of Nanjing University of Aeronautics & Astronautics,2015

4. Development overview and key technologies of high speed hybrid helicopter with single main rotor;Huang;Journal of Aerospace Power,2021

5. Research on propeller control strategy and coupling trimming method of the compound helicopter;Zhang;Flight Dynamics,2022

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