Spacecraft Combined Attitude and Sun Tracking (CAST) System.

The spacecraft solar panel Sun tracking mechanism is utilized as an attitude control system. This is done by manipulating the tracking control of both the solar panels along the spacecraft pitch axis to generate torque in order to counter-act the external disturbance along this axis. The two solar p...

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Main Authors: Varatharajoo, Renuganth, Allaudin, Mohd Faizal
Format: Article
Language:English
English
Published: 2011
Online Access:http://psasir.upm.edu.my/id/eprint/23345/1/Spacecraft%20Combined%20Attitude%20and%20Sun%20Tracking.pdf
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author Varatharajoo, Renuganth
Allaudin, Mohd Faizal
author_facet Varatharajoo, Renuganth
Allaudin, Mohd Faizal
author_sort Varatharajoo, Renuganth
collection UPM
description The spacecraft solar panel Sun tracking mechanism is utilized as an attitude control system. This is done by manipulating the tracking control of both the solar panels along the spacecraft pitch axis to generate torque in order to counter-act the external disturbance along this axis. The two solar panels are rotated at different speeds in order to generate the required torque. Matlab™ Simulink® was used to evaluate the system where the inputs are Sun tracking function and attitude reference while the outputs are the solar panel rotation angle due to Sun tracking and spacecraft’s pitch attitude. The governing equations together with the onboard attitude and solar tracking architecture are established. The architecture is the numerically tested. The simulation results are discussed especially from the attitude control standpoint. The integrated system complies very well with the reference mission requirement.
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spelling upm.eprints-233452015-10-07T04:45:47Z http://psasir.upm.edu.my/id/eprint/23345/ Spacecraft Combined Attitude and Sun Tracking (CAST) System. Varatharajoo, Renuganth Allaudin, Mohd Faizal The spacecraft solar panel Sun tracking mechanism is utilized as an attitude control system. This is done by manipulating the tracking control of both the solar panels along the spacecraft pitch axis to generate torque in order to counter-act the external disturbance along this axis. The two solar panels are rotated at different speeds in order to generate the required torque. Matlab™ Simulink® was used to evaluate the system where the inputs are Sun tracking function and attitude reference while the outputs are the solar panel rotation angle due to Sun tracking and spacecraft’s pitch attitude. The governing equations together with the onboard attitude and solar tracking architecture are established. The architecture is the numerically tested. The simulation results are discussed especially from the attitude control standpoint. The integrated system complies very well with the reference mission requirement. 2011 Article PeerReviewed application/pdf en http://psasir.upm.edu.my/id/eprint/23345/1/Spacecraft%20Combined%20Attitude%20and%20Sun%20Tracking.pdf Varatharajoo, Renuganth and Allaudin, Mohd Faizal (2011) Spacecraft Combined Attitude and Sun Tracking (CAST) System. Mathematics in Engineering, Science and Aerospace (MESA), 2 (4). pp. 413-421. ISSN 2041-3165 http://nonlinearstudies.com/index.php/mesa/article/view/629 English
spellingShingle Varatharajoo, Renuganth
Allaudin, Mohd Faizal
Spacecraft Combined Attitude and Sun Tracking (CAST) System.
title Spacecraft Combined Attitude and Sun Tracking (CAST) System.
title_full Spacecraft Combined Attitude and Sun Tracking (CAST) System.
title_fullStr Spacecraft Combined Attitude and Sun Tracking (CAST) System.
title_full_unstemmed Spacecraft Combined Attitude and Sun Tracking (CAST) System.
title_short Spacecraft Combined Attitude and Sun Tracking (CAST) System.
title_sort spacecraft combined attitude and sun tracking cast system
url http://psasir.upm.edu.my/id/eprint/23345/1/Spacecraft%20Combined%20Attitude%20and%20Sun%20Tracking.pdf
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