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...

وصف كامل

التفاصيل البيبلوغرافية
الحاوية / القاعدة:Journal of Aeronautics, Astronautics and Aviation
المؤلف الرئيسي: 2-s2.0-85104195789
التنسيق: مقال
اللغة:English
منشور في: The Aeronautical and Astronautical Society of the Republic of China 2021
الوصول للمادة أونلاين: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