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|Title:||Design and assembling of a UAV helicopter system||Authors:||Cai, G.
|Issue Date:||2005||Citation:||Cai, G.,Peng, K.,Chen, B.M.,Lee, T.H. (2005). Design and assembling of a UAV helicopter system. Proceedings of the 5th International Conference on Control and Automation, ICCA'05 : 697-702. ScholarBank@NUS Repository.||Abstract:||A simple UAV helicopter is to be constructed as a test bed for the implementation of some newly developed nonlinear control technologies. The UAV helicopter consists of (a) an advanced toy radio-controlled helicopter as a basic aircraft; (b) a simple avionic system to be developed; and (c) a ground supporting system. The avionic system includes a miniature PC-104 computer system (airborne) and a MEMS (mechanical and electrical micro system) navigation and inertial measurement unit as a major sensing unit. A couple of full duplex transceivers are used to provide wireless communications between the helicopter and the ground unit. The ground transceiver and a computer system stationed in the ground form a supporting system. The UAV helicopter is to be used to implement automatic ight control systems. © 2005 IEEE.||Source Title:||Proceedings of the 5th International Conference on Control and Automation, ICCA'05||URI:||http://scholarbank.nus.edu.sg/handle/10635/69820||ISBN:||0780391381|
|Appears in Collections:||Staff Publications|
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