Satellite attitude tracking control using Lyapunov control theory

Okasha, Mohamed Elsayed Aly Abd Elaziz and Idres, Moumen and Ghaffar, Alia (2019) Satellite attitude tracking control using Lyapunov control theory. International Journal of Recent Technology and Engineering (IJRTE), 7 (6S). pp. 253-257. ISSN 2277-3878

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Abstract

This paper explores attitude control algorithms using thrusters and momentum wheels for satellite tracking manoeuver. The attitude reference trajectory is generated to track a ground object on the rotating Earth and to keep the Sun vector perpendicular to the solar panel to maximize the solar power. The dynamic model is derived based on Newton-Euler approach and Modified Rodrigues Parameters (MRPs) are used to represent attitude kinematics. The control algorithms are derived based on the Lyapunov stability control theory to ensure the asymptotic stability of the control law. MATLAB software package is used as a simulation environment to develop and test the performance of the proposed tracking control algorithms using a Graphical User Interface (GUI) tool that can be expanded for future development.

Item Type:	Article (Journal)
Additional Information:	6908/74025
Uncontrolled Keywords:	Attitude tracking; Lyapunov stability; Satellite dynamics and control
Subjects:	T Technology > TL Motor vehicles. Aeronautics. Astronautics T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL500 Aeronautics T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL787 Astronautics
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button):	Kulliyyah of Engineering > Department of Mechanical Engineering Kulliyyah of Engineering
Depositing User:	Dr Mohamed Okasha
Date Deposited:	12 Sep 2019 15:09
Last Modified:	12 Sep 2019 15:09
URI:	http://irep.iium.edu.my/id/eprint/74025

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