The Proceedings of the Symposium on the Motion and Vibration Control
Online ISSN : 2424-3000
2003.8
Conference information
Helicopter Attitude Control with a Nonlinear Internal Model Control
Ryo KIYOFUJIShinichiro SAITOKatsutoshi TAMURA
Author information
CONFERENCE PROCEEDINGS FREE ACCESS

Pages 550-553

Details
Abstract
In this paper, we introduce a method for controlling a nonlinear helicopter model. The method is constructed by controlling the internal model of the helicopter model by backstepping control, so that the plant follows the input of the whole system. We first show in this paper the modeling of the helicopter system, second we describe the designed control system, and at last we show the simulation results and find that this method has effectiveness.
Content from these authors
© 2003 The Japan Society of Mechanical Engineers
Previous article Next article
feedback
Top