Analysis of Airframe Parameters of OAT-bicopter to Optimize Pitch Stability-Reference-Cited by-同舟云学术

Analysis of Airframe Parameters of OAT-bicopter to Optimize Pitch Stability

Published:2023-05-12 Issue: Volume: Page:
ISSN:
Container-title:Proceedings of the 2023 3rd International Conference on Robotics and Control Engineering
language:
Short-container-title:

Author:

Xu Junsheng¹^ORCID,Yu Chengxiang¹^ORCID,Li Heqing²^ORCID,Zhao Chenyang³^ORCID,Li Qijun¹^ORCID,Li Xinde⁴^ORCID

Affiliation:

1. School of Automation, Southeast University, China

2. School of Cyber Science and Engineering, Southeast University, China

3. School of Software Engineering, Southeast University, China

4. School of Automation, Southeast University, China and Nanjing Center for Applied Mathematics, China

Funder

Key Projects of Key R&D Program of Jiangsu Province

National Natural Science Foundation of China

Shenzhen Natural Science Foundation

Publisher

ACM

Link

https://dl.acm.org/doi/pdf/10.1145/3598151.3598434

Reference16 articles.

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4. Triple tilting rotor mini-UAV: Modeling and embedded control of the attitude

5. Ranjan Ganguli , Beatrix Jehnert , Jens Wolfram , and Peter Voersmann . 2007. Optimal location of centre of gravity for swashplateless helicopter UAV and MAV. Aircraft Engineering and Aerospace Technology ( 2007 ). Ranjan Ganguli, Beatrix Jehnert, Jens Wolfram, and Peter Voersmann. 2007. Optimal location of centre of gravity for swashplateless helicopter UAV and MAV. Aircraft Engineering and Aerospace Technology (2007).