UAV Dynamic Behaviour Comparison of Quadcopter Based on Thrust Differential and Tilted Rotor

UAV Dynamic Behaviour Comparison of Quadcopter Based on Thrust Differential and Tilted Rotor

This paper describes the comparison of dynamic behavior of quadcopter between thrust differential and tilted rotor. The difference of thrust is acquired by applying unequal thrust among front and aft rotors while the tilted rotor has a control mechanism by tilting the rotors. The equations of motion...

詳細記述

書誌詳細
出版年:Journal of Aeronautics, Astronautics and Aviation
第一著者: 2-s2.0-85104195789
フォーマット: 論文
言語:English
出版事項: The Aeronautical and Astronautical Society of the Republic of China 2021
オンライン･アクセス:https://www.scopus.com/inward/record.uri?eid=2-s2.0-85104195789&doi=10.6125%2fJoAAA.202106_53%282%29.18&partnerID=40&md5=180a95e7e368a36244bdc253193f6380

インターネット

https://www.scopus.com/inward/record.uri?eid=2-s2.0-85104195789&doi=10.6125%2fJoAAA.202106_53%282%29.18&partnerID=40&md5=180a95e7e368a36244bdc253193f6380

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