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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/14945/1/Integrated_Attitude_Determination.pdf
http://irep.iium.edu.my/14945/
http://www.wseas.us/e-library/conferences/2009/istanbul/ACMOS/ACMOS-38.pdf
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spelling my.iium.irep.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 REM 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
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
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/14945/1/Integrated_Attitude_Determination.pdf
http://irep.iium.edu.my/14945/
http://www.wseas.us/e-library/conferences/2009/istanbul/ACMOS/ACMOS-38.pdf
_version_ 1643606955309137920
score 13.211869

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