Assessment of earth remote sensing microsatellite power subsystem sapability during detumbling and nominal modes

The Electric Power Subsystem (EPS) is one of the most critical systems on any satellite because nearly every subsystem requires power. This makes the choice of power systems the most important task facing satellite designers. The main purpose of the Satellite EPS is to provide continuous, regulated...

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Main Authors:	Zahran, Mohamed, Okasha, Mohamed Elsayed Aly Abd Elaziz, Ivanova, Galina A.
Format:	Article
Language:	English
Published:	Korean Institute of Power Electronics 2006
Subjects:	TA168 Systems engineering TA329 Engineering mathematics. Engineering analysis TA349 Mechanics of engineering. Applied mechanics
Online Access:	http://irep.iium.edu.my/38710/ http://irep.iium.edu.my/38710/ http://irep.iium.edu.my/38710/1/JPE_6-1-3.pdf

id	iium-38710
recordtype	eprints
spelling	iium-387102014-10-15T01:51:28Z http://irep.iium.edu.my/38710/ Assessment of earth remote sensing microsatellite power subsystem sapability during detumbling and nominal modes Zahran, Mohamed Okasha, Mohamed Elsayed Aly Abd Elaziz Ivanova, Galina A. TA168 Systems engineering TA329 Engineering mathematics. Engineering analysis TA349 Mechanics of engineering. Applied mechanics The Electric Power Subsystem (EPS) is one of the most critical systems on any satellite because nearly every subsystem requires power. This makes the choice of power systems the most important task facing satellite designers. The main purpose of the Satellite EPS is to provide continuous, regulated and conditioned power to all the satellite subsystems. It has to withstand radiation, thermal cycling and vacuums in hostile space environments, as well as subsystem degradation over time. The EPS power characteristics are determined by both the parameters of the system itself and by the satellite orbit. After satellite separation from the launch vehicle (LV) to its orbit, in almost all situations, the satellite subsystems (attitude determination and control, communication and onboard computer and data handling (OBC&DH)), take their needed power from a storage battery (SB) and solar arrays (SA) besides the consumed power in the EPS management device. At this point (separation point, detumbling mode), the satellite’s angular motion is high and the orientation of the solar arrays, with respect to the Sun, will change in a non-uniform way, so the amount of power generated by the solar arrays will be affected. The objective of this research is to select satellite EPS component types, to estimate solar array illumination parameters and to determine the efficiency of solar arrays during both detumbling and normal operation modes. Korean Institute of Power Electronics 2006 Article PeerReviewed application/pdf en http://irep.iium.edu.my/38710/1/JPE_6-1-3.pdf Zahran, Mohamed and Okasha, Mohamed Elsayed Aly Abd Elaziz and Ivanova, Galina A. (2006) Assessment of earth remote sensing microsatellite power subsystem sapability during detumbling and nominal modes. Journal of Power Electronics, 6 (1). pp. 18-28. ISSN 1598-2092 http://review.jpe.or.kr/On_line/admin/paper/files/JPE%206-1-3.pdf
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English
topic	TA168 Systems engineering TA329 Engineering mathematics. Engineering analysis TA349 Mechanics of engineering. Applied mechanics
spellingShingle	TA168 Systems engineering TA329 Engineering mathematics. Engineering analysis TA349 Mechanics of engineering. Applied mechanics Zahran, Mohamed Okasha, Mohamed Elsayed Aly Abd Elaziz Ivanova, Galina A. Assessment of earth remote sensing microsatellite power subsystem sapability during detumbling and nominal modes
description	The Electric Power Subsystem (EPS) is one of the most critical systems on any satellite because nearly every subsystem requires power. This makes the choice of power systems the most important task facing satellite designers. The main purpose of the Satellite EPS is to provide continuous, regulated and conditioned power to all the satellite subsystems. It has to withstand radiation, thermal cycling and vacuums in hostile space environments, as well as subsystem degradation over time. The EPS power characteristics are determined by both the parameters of the system itself and by the satellite orbit. After satellite separation from the launch vehicle (LV) to its orbit, in almost all situations, the satellite subsystems (attitude determination and control, communication and onboard computer and data handling (OBC&DH)), take their needed power from a storage battery (SB) and solar arrays (SA) besides the consumed power in the EPS management device. At this point (separation point, detumbling mode), the satellite’s angular motion is high and the orientation of the solar arrays, with respect to the Sun, will change in a non-uniform way, so the amount of power generated by the solar arrays will be affected. The objective of this research is to select satellite EPS component types, to estimate solar array illumination parameters and to determine the efficiency of solar arrays during both detumbling and normal operation modes.
format	Article
author	Zahran, Mohamed Okasha, Mohamed Elsayed Aly Abd Elaziz Ivanova, Galina A.
author_facet	Zahran, Mohamed Okasha, Mohamed Elsayed Aly Abd Elaziz Ivanova, Galina A.
author_sort	Zahran, Mohamed
title	Assessment of earth remote sensing microsatellite power subsystem sapability during detumbling and nominal modes
title_short	Assessment of earth remote sensing microsatellite power subsystem sapability during detumbling and nominal modes
title_full	Assessment of earth remote sensing microsatellite power subsystem sapability during detumbling and nominal modes
title_fullStr	Assessment of earth remote sensing microsatellite power subsystem sapability during detumbling and nominal modes
title_full_unstemmed	Assessment of earth remote sensing microsatellite power subsystem sapability during detumbling and nominal modes
title_sort	assessment of earth remote sensing microsatellite power subsystem sapability during detumbling and nominal modes
publisher	Korean Institute of Power Electronics
publishDate	2006
url	http://irep.iium.edu.my/38710/ http://irep.iium.edu.my/38710/ http://irep.iium.edu.my/38710/1/JPE_6-1-3.pdf
first_indexed	2023-09-18T20:55:39Z
last_indexed	2023-09-18T20:55:39Z
_version_	1777410285586350080

Assessment of earth remote sensing microsatellite power subsystem sapability during detumbling and nominal modes

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