Please use this identifier to cite or link to this item:
|Title:||Design of a PI-D Controller of a Scaled-Model Helicopter||Authors:||Abiad, Hassan El
|Affiliations:||Department of Electrical Engineering||Keywords:||Three-term control
|Subjects:||Helicopters||Issue Date:||2006||Part of:||WSEAS transactions on systems||Volume:||9||Issue:||5||Start page:||2120||End page:||2125||Abstract:||
Scaled-model helicopters are highly nonlinear, coupled, and unstable machines. They have fast response and controlling them is very complicated and need high degree of precision. In this paper, a detailed nonlinear model is derived. The derived nonlinear model is linearized around a nominal point in the hovering state and a linear classical controller is designed. Then, an optimization algorithm is applied where the linear controller's parameters are adjusted offline so that the Integral Time-multiplied Square Error (ITSE), the error between the output response of the nonlinear system and the reference signal, is minimal. Both the linear and the optimized controllers are augmented with the nonlinear model and the simulation results are compared.
This paper was presented in " Proceedings of the 10th WSEAS International Conference on Systems, Vouliagmeni, Athens, Greece, July 10-12, 2006 ".
|URI:||https://scholarhub.balamand.edu.lb/handle/uob/1829||Open URL:||Link to full text||Type:||Journal Article|
|Appears in Collections:||Department of Electrical Engineering|
Show full item record
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.