An integrator backstepping controller for a standard helicopter
type: CreativeWork
description: This thesis investigates the use of an integrator backstepping controller for a standard helicopter. First, a dynamic model of the helicopter in hovering condition is obtained through the use of Newton-Euler equations. Next, the idea of an integrator backstepping controller is examined followed by the derivation of the actual controller. Finally, simulation results from MATLAB are analyzed and potential future work is proposed.
abstract: This thesis investigates the use of an integrator backstepping controller for a standard helicopter. First, a dynamic model of the helicopter in hovering condition is obtained through the use of Newton-Euler equations. Next, the idea of an integrator backstepping controller is examined followed by the derivation of the actual controller. Finally, simulation results from MATLAB are analyzed and potential future work is proposed.
author: Liu, Yitao
language: en
keywords: integrator backstepping controller, standard helicopter model
date published: 2010-08-20T17:58:46Z
date modified: 2026-07-22T22:25:09Z
provider: University of Illinois - Urbana-Champaign
publisher: Networked Digital Library of Theses and Dissertations
type: WebPage
source organization: University of Illinois at Urbana-Champaign

PropertyValue
property ID: Handle
value: http://hdl.handle.net/2142/16818