Paper
25 October 2023 Research on pitch angle control of a small moving-mass tail-sitter UAV with moving load
Qiangqiang Chen, Lei He
Author Affiliations +
Proceedings Volume 12801, Ninth International Conference on Mechanical Engineering, Materials, and Automation Technology (MMEAT 2023); 128014E (2023) https://doi.org/10.1117/12.3007287
Event: Ninth International Conference on Mechanical Engineering, Materials, and Automation Technology (MMEAT 2023), 2023, Dalian, China
Abstract
This paper designs a tail-sitter UAV that combines the advantages of a fixed-wing UAV and a rotary-wing UAV. Based on the designed model, a study that the attitude of the moving-mass UAV under the different conditions of the moving load in the horizontal cruise phase is carried out. The results show that the stability of the flight attitude of the whole aircraft in the cruise phase is verified. And the study is essential to ensure the safety of the whole tail-sitter UAV.
(2023) Published by SPIE. Downloading of the abstract is permitted for personal use only.
Qiangqiang Chen and Lei He "Research on pitch angle control of a small moving-mass tail-sitter UAV with moving load", Proc. SPIE 12801, Ninth International Conference on Mechanical Engineering, Materials, and Automation Technology (MMEAT 2023), 128014E (25 October 2023); https://doi.org/10.1117/12.3007287
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KEYWORDS
Unmanned aerial vehicles

Control systems

Angular velocity

Mathematical modeling

Simulink

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