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|Title:||Modeling and control system design for a UAV helicopter||Authors:||Cai, G.
|Issue Date:||2006||Citation:||Cai, G.,Chen, B.M.,Peng, K.,Dong, M.,Lee, T.H. (2006). Modeling and control system design for a UAV helicopter. 14th Mediterranean Conference on Control and Automation, MED'06 : -. ScholarBank@NUS Repository. https://doi.org/10.1109/MED.2006.328860||Abstract:||We present in this paper a linearized hovering model of a UAV helicopter obtained using the in-flight data generated through a perturbation method. The UAV helicopter is constructed from a radio-controlled helicopter by integrating an onboard system, which includes a data processing unit, a data acquisition system, a wireless communications and all necessary sensors. A flight control law is then designed using a newly developed nonlinear control technique, i.e. the composite nonlinear feedback control. Actual flight testing shows that the design is successful.||Source Title:||14th Mediterranean Conference on Control and Automation, MED'06||URI:||http://scholarbank.nus.edu.sg/handle/10635/70983||ISBN:||0978672003||DOI:||10.1109/MED.2006.328860|
|Appears in Collections:||Staff Publications|
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