Design, control, aerodynamic performances, and structural integrity investigations of compact ducted drone with co-axial propeller for high altitude surveillance

Abstract Compact multi-rotor unmanned aerial vehicles (UAVs) can be operated in many challenging environmental conditions. In case the UAV requires certain considerations in designing like lightweight, efficient propulsion system and others depending upon the application, the hybrid UAV comes into p...

وصف كامل

التفاصيل البيبلوغرافية

المؤلفون الرئيسيون:	Shyam Sundar Jayakumar, Indira Prasanth Subramaniam, Beena Stanislaus Arputharaj, Senthil Kumar Solaiappan, Parvathy Rajendran, It Ee Lee, Senthil Kumar Madasamy, Raj Kumar Gnanasekaran, Arunkumar Karuppasamy, Vijayanandh Raja
التنسيق:	Artigo
اللغة:	Inglês
منشور في:	Nature Portfolio 2024-03-01
سلاسل:	Scientific Reports
الموضوعات:	Attitude control Bi-copter Composite materials Ducted Drone CFD FEA
الوصول للمادة أونلاين:	https://doi.org/10.1038/s41598-024-54174-x
الوسوم:	إضافة وسم لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!