Please use this identifier to cite or link to this item:
|Title:||Modeling and control system design for a UAV helicopter|
|Authors:||Cai, G. |
|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|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on Jan 16, 2019
checked on Jan 12, 2019
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.