Spacecraft attitude control: development and application of new algorithms

Abdelrahman, Mohammad and Hassan, Sayed (2012) Spacecraft attitude control: development and application of new algorithms. LAMBERT Academic Publishing, Germany. ISBN 978-3848400867

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Abstract

The main goal of the research is to collect and develop new attitude algorithms that build up the different scenarios acted by a spacecraft starting from the orbit injection phase. It is found that the attitude scenarios can be classified mainly into two categories the first is the angular momentum management of a spacecraft and the second is the attitude maneuvers. The first category can be divided into two modes which are the detumbling mode and the momentum unloading mode. A new algorithm for estimating the angular rates has been developed. In the second category, the attitude maneuver, the research work is concluded by developing a new technique to solve the problem of the second category using neuro-fuzzy control.

Item Type:	Book
Additional Information:	6540/23041
Subjects:	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
Depositing User:	Dr. Mohammad Abdelrahman
Date Deposited:	25 May 2012 14:47
Last Modified:	25 May 2012 14:47
URI:	http://irep.iium.edu.my/id/eprint/23041

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