Please use this identifier to cite or link to this item: https://doi.org/10.1109/MED.2006.328860
Title: Modeling and control system design for a UAV helicopter
Authors: Cai, G. 
Chen, B.M. 
Peng, K. 
Dong, M. 
Lee, T.H. 
Issue Date: 2006
Source: 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
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