A Study on High Agile Satellite Maneuver using Reaction Wheels and CMGs
In: Journal of the Korean Society for Aeronautical & Space Sciences, Jg. 41 (2013-02-01), S. 107-119
Online
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Zugriff:
We study three axis attitude control method including two axis high agile maneuver using four reaction wheels and two control moment gyros. We investigate singularity conditions due to two control moment gyros and propose singularity escape method. Based on this, we propose actuator control algorithm for high agile maneuver. Also, we propose actuator momentum management method which preserves momentum of reaction wheels and control moment gyroscopes before and after satellite attitude control. Through numerical simulation, we show that our method achieves three axis attitude control including two axis high agile maneuver and preserves actuators' momentum.
Titel: |
A Study on High Agile Satellite Maneuver using Reaction Wheels and CMGs
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Autor/in / Beteiligte Person: | Son, Jun-Won ; Rhee, Seung-Wu |
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Zeitschrift: | Journal of the Korean Society for Aeronautical & Space Sciences, Jg. 41 (2013-02-01), S. 107-119 |
Veröffentlichung: | The Korean Society for Aeronautical & Space Sciences, 2013 |
Medientyp: | unknown |
ISSN: | 1225-1348 (print) |
DOI: | 10.5139/jksas.2013.41.2.107 |
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