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|Title:||Modeling and control system design for a UAV helicopter|
|Authors:||Cai, G. |
|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|
|Appears in Collections:||Staff Publications|
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