DocumentCode
693019
Title
The application requirement analysis and system design of shipborne small multi-rotors unmanned aerial vehicle
Author
Fan SongWei ; Bian HongWei
Author_Institution
Dept. of Navig., Electr. Eng. Acad., Naval Univ. of Eng., Wuhan, China
fYear
2013
fDate
20-22 Dec. 2013
Firstpage
2812
Lastpage
2816
Abstract
The small multi-rotors unmanned aerial vehicle (UAV) fits for complex narrow ship environment. Using it could improve the efficiency of the lots of ship task. The tasks include the carry mission and video mission could be performed by the small multi-rotors UAV. According to the mission requirements: low weight, small size, antivibration, low power consumption, and easy interfacing, the vehicle system is designed in four subsystems: flight power subsystem, long-range wireless data link subsystem, flight control subsystem and ground control subsystem. The model vehicle is constructed and the flying experiment shows that the model vehicle could realize steady flight and Airline flight, meets the design requirements.
Keywords
autonomous aerial vehicles; rotors; UAV; airline flight; carry mission; design requirements; flight control subsystem; flight power subsystem; ground control subsystem; long-range wireless data link subsystem; mission requirements; ship environment; ship task; shipborne small multi-rotors unmanned aerial vehicle; steady flight; video mission; Aircraft; Aircraft propulsion; Humidity measurement; Magnetic field measurement; Navigation; Size measurement; Weight measurement; application requirement analysis; shipborne multi-rotors; system design;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronic Sciences, Electric Engineering and Computer (MEC), Proceedings 2013 International Conference on
Conference_Location
Shengyang
Print_ISBN
978-1-4799-2564-3
Type
conf
DOI
10.1109/MEC.2013.6885508
Filename
6885508
Link To Document