Model and control on the ascending process of rotating wing helicopter

The aim of this research project is to develop an autopilot system that enables the helicopter model to carry out autonomous hover manoeuvre using on-board intelligence computer. The main goal of this project is to provide a comprehensive design methodology, implementation and testing of an autopi...

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Main Author:	Noor Zalika , Kornain
Format:	Undergraduates Project Papers
Language:	English
Published:	2013
Subjects:	TJ Mechanical engineering and machinery
Online Access:	http://umpir.ump.edu.my/id/eprint/7670/ http://umpir.ump.edu.my/id/eprint/7670/ http://umpir.ump.edu.my/id/eprint/7670/1/NOOR_ZALIKA_KORNAIN.PDF

id	ump-7670
recordtype	eprints
spelling	ump-76702015-03-03T09:37:24Z http://umpir.ump.edu.my/id/eprint/7670/ Model and control on the ascending process of rotating wing helicopter Noor Zalika , Kornain TJ Mechanical engineering and machinery The aim of this research project is to develop an autopilot system that enables the helicopter model to carry out autonomous hover manoeuvre using on-board intelligence computer. The main goal of this project is to provide a comprehensive design methodology, implementation and testing of an autopilot system developed for a rotorcraft-based unmanned aerial vehicles (UAV). The autopilot system was designed to demonstrate autonomous manoeuvres such as take-off and hovering flight capabilities. For the controller design, the nonlinear dynamic model of the helicopter was built comprising of four different subsystems such as actuators dynamics, rotary wings dynamics, force and moment generation process and rigid body dynamics. Stabilization of the helicopter was derived by using Proportional Integral Derivative method. The overall system consists of the helicopter with an on-board computer and a second computer serving as a ground station. While flight control is done on-board, mission planning and human user interaction take place on ground. Sensors used for autonomous operation include acceleration and euler angles sensors The hardware and software used to autonomously pilot the helicopter were described in detailed in this thesis. Series of test flight were conducted to verify autopilot system performance. The proposed hovering controller has shown capable of stabilizing the helicopter attitude angles. 2013-09 Undergraduates Project Papers NonPeerReviewed application/pdf en http://umpir.ump.edu.my/id/eprint/7670/1/NOOR_ZALIKA_KORNAIN.PDF Noor Zalika , Kornain (2013) Model and control on the ascending process of rotating wing helicopter. Faculty of Manufacturing Engineering, Universiti Malaysia Pahang. http://iportal.ump.edu.my/lib/item?id=chamo:78503&theme=UMP2
repository_type	Digital Repository
institution_category	Local University
institution	Universiti Malaysia Pahang
building	UMP Institutional Repository
collection	Online Access
language	English
topic	TJ Mechanical engineering and machinery
spellingShingle	TJ Mechanical engineering and machinery Noor Zalika , Kornain Model and control on the ascending process of rotating wing helicopter
description	The aim of this research project is to develop an autopilot system that enables the helicopter model to carry out autonomous hover manoeuvre using on-board intelligence computer. The main goal of this project is to provide a comprehensive design methodology, implementation and testing of an autopilot system developed for a rotorcraft-based unmanned aerial vehicles (UAV). The autopilot system was designed to demonstrate autonomous manoeuvres such as take-off and hovering flight capabilities. For the controller design, the nonlinear dynamic model of the helicopter was built comprising of four different subsystems such as actuators dynamics, rotary wings dynamics, force and moment generation process and rigid body dynamics. Stabilization of the helicopter was derived by using Proportional Integral Derivative method. The overall system consists of the helicopter with an on-board computer and a second computer serving as a ground station. While flight control is done on-board, mission planning and human user interaction take place on ground. Sensors used for autonomous operation include acceleration and euler angles sensors The hardware and software used to autonomously pilot the helicopter were described in detailed in this thesis. Series of test flight were conducted to verify autopilot system performance. The proposed hovering controller has shown capable of stabilizing the helicopter attitude angles.
format	Undergraduates Project Papers
author	Noor Zalika , Kornain
author_facet	Noor Zalika , Kornain
author_sort	Noor Zalika , Kornain
title	Model and control on the ascending process of rotating wing helicopter
title_short	Model and control on the ascending process of rotating wing helicopter
title_full	Model and control on the ascending process of rotating wing helicopter
title_fullStr	Model and control on the ascending process of rotating wing helicopter
title_full_unstemmed	Model and control on the ascending process of rotating wing helicopter
title_sort	model and control on the ascending process of rotating wing helicopter
publishDate	2013
url	http://umpir.ump.edu.my/id/eprint/7670/ http://umpir.ump.edu.my/id/eprint/7670/ http://umpir.ump.edu.my/id/eprint/7670/1/NOOR_ZALIKA_KORNAIN.PDF
first_indexed	2023-09-18T22:04:31Z
last_indexed	2023-09-18T22:04:31Z
_version_	1777414618873856000

Model and control on the ascending process of rotating wing helicopter

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