Integrated attitude determination and control system via magnetic measurements and actuation only

A nonlinear control scheme using a Modified State–Dependent Riccati Equation MSDRE has been developed through a pseudo-linearization of spacecraft augmented dynamics and kinematics. The full-state knowledge, required for the control loop is provided through a generalized algorithm for spacecraft...

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Main Authors:	Mohammad Abdel Rahman, Mohammad Ibraheem, Sang-Young, Park
Format:	Conference or Workshop Item
Language:	English
Published:	2009
Subjects:	TA Engineering (General). Civil engineering (General)
Online Access:	http://irep.iium.edu.my/14945/ http://irep.iium.edu.my/14945/ http://irep.iium.edu.my/14945/1/Integrated_Attitude_Determination.pdf

id	iium-14945
recordtype	eprints
spelling	iium-149452013-07-01T07:08:17Z http://irep.iium.edu.my/14945/ Integrated attitude determination and control system via magnetic measurements and actuation only Mohammad Abdel Rahman, Mohammad Ibraheem Sang-Young, Park TA Engineering (General). Civil engineering (General) A nonlinear control scheme using a Modified State–Dependent Riccati Equation MSDRE has been developed through a pseudo-linearization of spacecraft augmented dynamics and kinematics. The full-state knowledge, required for the control loop is provided through a generalized algorithm for spacecraft three-axis attitude and rate estimation based on the utilization of magnetometer measurements and their time derivatives, while the control torque is generated via magnetorquers. The resulted attitude determination and control system has shown the capability of estimating the attitude better than 5 deg and rate of order 0.03 deg/sec in addition to maintain the pointing accuracy within 5 deg in each axis with pointing stability of less than 0.05 deg/sec. 2009 Conference or Workshop Item NonPeerReviewed application/pdf en http://irep.iium.edu.my/14945/1/Integrated_Attitude_Determination.pdf Mohammad Abdel Rahman, Mohammad Ibraheem and Sang-Young, Park (2009) Integrated attitude determination and control system via magnetic measurements and actuation only. In: Proceedings of the 11th WSEAS International Conference on Automatic Control, Modelling and Simulation (ACMOS 2009), 30th May - 1st Jun 2009, Instanbul, Turkey. http://www.wseas.us/e-library/conferences/2009/istanbul/ACMOS/ACMOS-38.pdf
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English
topic	TA Engineering (General). Civil engineering (General)
spellingShingle	TA Engineering (General). Civil engineering (General) Mohammad Abdel Rahman, Mohammad Ibraheem Sang-Young, Park Integrated attitude determination and control system via magnetic measurements and actuation only
description	A nonlinear control scheme using a Modified State–Dependent Riccati Equation MSDRE has been developed through a pseudo-linearization of spacecraft augmented dynamics and kinematics. The full-state knowledge, required for the control loop is provided through a generalized algorithm for spacecraft three-axis attitude and rate estimation based on the utilization of magnetometer measurements and their time derivatives, while the control torque is generated via magnetorquers. The resulted attitude determination and control system has shown the capability of estimating the attitude better than 5 deg and rate of order 0.03 deg/sec in addition to maintain the pointing accuracy within 5 deg in each axis with pointing stability of less than 0.05 deg/sec.
format	Conference or Workshop Item
author	Mohammad Abdel Rahman, Mohammad Ibraheem Sang-Young, Park
author_facet	Mohammad Abdel Rahman, Mohammad Ibraheem Sang-Young, Park
author_sort	Mohammad Abdel Rahman, Mohammad Ibraheem
title	Integrated attitude determination and control system via magnetic measurements and actuation only
title_short	Integrated attitude determination and control system via magnetic measurements and actuation only
title_full	Integrated attitude determination and control system via magnetic measurements and actuation only
title_fullStr	Integrated attitude determination and control system via magnetic measurements and actuation only
title_full_unstemmed	Integrated attitude determination and control system via magnetic measurements and actuation only
title_sort	integrated attitude determination and control system via magnetic measurements and actuation only
publishDate	2009
url	http://irep.iium.edu.my/14945/ http://irep.iium.edu.my/14945/ http://irep.iium.edu.my/14945/1/Integrated_Attitude_Determination.pdf
first_indexed	2023-09-18T20:24:01Z
last_indexed	2023-09-18T20:24:01Z
_version_	1777408295872495616

Integrated attitude determination and control system via magnetic measurements and actuation only

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