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Modelling and control of flexible structure for satellite attitude maneuvers using pole placement and PID controller

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Bibliographic Details
Main Author: Muhamad Asraf, Basharudin
Other Authors: Che Muhammad Nor Che Isa
Format: Learning Object
Language:English
Published: Universiti Malaysia Perlis (UniMAP) 2016
Subjects:
Satellite
Satellite attitude maneuver
Satellite (solar panel)
Satellite attitude maneuver > Design and construction
Online Access:http://dspace.unimap.edu.my:80/xmlui/handle/123456789/41830
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spelling my.unimap-418302016-06-02T09:16:31Z Modelling and control of flexible structure for satellite attitude maneuvers using pole placement and PID controller Muhamad Asraf, Basharudin Che Muhammad Nor Che Isa Satellite Satellite attitude maneuver Satellite (solar panel) Satellite attitude maneuver -- Design and construction Access is limited to UniMAP community. This thesis describes the studies on vibration of flexible structure of satellite (solar panel) by using cantilever beam for performance analysis. Nearly ideal cantilever beam model is studied to provide basic understanding in vibration solar panel of satellite operation, follow by a mathematical model of cantilever beam, containing relationships for vibration reaction, angular momentum, power consumption and disturbances. From the cantilever model with consist of parameters to studies about response on vibration. To solve this problem, MATLAB/SIMULINK is used to obtain the transfer function of the cantilever beam modeling. From simulation results shows a transfer function modeling providing the slow time response. For this case, fast response controller design was implemented in this modeling. Pole Placement controller and PID controller are designed and compared the performance on the modeling system by using MATLAB/SIMULINK. Simulation results show PID adding Pole Placement controller gives better performance in term of rise time, settling time, percentage overshoot, steady state error and performance indices than Pole Placement controller. 2016-06-02T09:16:31Z 2016-06-02T09:16:31Z 2015-06 Learning Object http://dspace.unimap.edu.my:80/xmlui/handle/123456789/41830 en Universiti Malaysia Perlis (UniMAP) School of Computer and Communication Engineering
institution Universiti Malaysia Perlis
building UniMAP Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Malaysia Perlis
content_source UniMAP Library Digital Repository
url_provider http://dspace.unimap.edu.my/
language English
topic Satellite
Satellite attitude maneuver
Satellite (solar panel)
Satellite attitude maneuver -- Design and construction
spellingShingle Satellite
Satellite attitude maneuver
Satellite (solar panel)
Satellite attitude maneuver -- Design and construction
Muhamad Asraf, Basharudin
Modelling and control of flexible structure for satellite attitude maneuvers using pole placement and PID controller
description Access is limited to UniMAP community.
author2 Che Muhammad Nor Che Isa
author_facet Che Muhammad Nor Che Isa
Muhamad Asraf, Basharudin
format Learning Object
author Muhamad Asraf, Basharudin
author_sort Muhamad Asraf, Basharudin
title Modelling and control of flexible structure for satellite attitude maneuvers using pole placement and PID controller
title_short Modelling and control of flexible structure for satellite attitude maneuvers using pole placement and PID controller
title_full Modelling and control of flexible structure for satellite attitude maneuvers using pole placement and PID controller
title_fullStr Modelling and control of flexible structure for satellite attitude maneuvers using pole placement and PID controller
title_full_unstemmed Modelling and control of flexible structure for satellite attitude maneuvers using pole placement and PID controller
title_sort modelling and control of flexible structure for satellite attitude maneuvers using pole placement and pid controller
publisher Universiti Malaysia Perlis (UniMAP)
publishDate 2016
url http://dspace.unimap.edu.my:80/xmlui/handle/123456789/41830
_version_ 1643799820334268416
score 13.145442

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