A Novel Heli-Twin-Rotor Unmanned Aerial Vehicle: Design, Realization and Flying
This paper presents a novel twin-rotor Unmanned Aerial Vehicle (UAV). By replacing the conventional single swashplate with two independent tilting mechanisms, it simplifies the mechanical structure and achieves control decoupling, while also mitigating aerodynamic coupling.
Authors
- Jing Sun (ORCID: https://orcid.org/0000-0002-1223-8986)
- Shuijing Wu (ORCID: https://orcid.org/0000-0001-8898-2667)
- Xiuwen Fu (ORCID: https://orcid.org/0000-0001-5611-3504)
- Zhi Chen (ORCID: https://orcid.org/0000-0002-9307-4871)
- Jing Ma (ORCID: https://orcid.org/0000-0003-0103-9858)
- Jiajun Fu (ORCID: https://orcid.org/0000-0003-4819-3377)
Institutions
- Shanghai University (CN)
Publication Details
- Journal
- Guidance Navigation and Control
- Published
- 2025-11-03
- DOI
- https://doi.org/10.1142/s2737480725500426
- Primary Topic
- Biomimetic flight and propulsion mechanisms
- Type
- article
- Field-Weighted Citation Impact
- 0.00