Reaction Wheel Disturbance Reduction Method Using Disturbance Measurement Table

Momentum changing actuators like reaction wheels and control moment gyros are generally used for spacecraft attitude control. This type of actuators produces force and torque disturbances. These disturbances must be reduced since they degrade the quality of spacecraft attitude control. Major distu...

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Main Authors: Dong-Ik Cheon, Eun-Jeong Jang, Hwa-Suk Oh
Format: Article
Language:English
Published: The Korean Space Science Society 2011-12-01
Series:Journal of Astronomy and Space Sciences
Subjects:
Online Access:http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2011/v28n4/OJOOBS_2011_v28n4_311.pdf
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author Dong-Ik Cheon
Eun-Jeong Jang
Hwa-Suk Oh
author_facet Dong-Ik Cheon
Eun-Jeong Jang
Hwa-Suk Oh
author_sort Dong-Ik Cheon
collection DOAJ
description Momentum changing actuators like reaction wheels and control moment gyros are generally used for spacecraft attitude control. This type of actuators produces force and torque disturbances. These disturbances must be reduced since they degrade the quality of spacecraft attitude control. Major disturbances are mainly due to static and dynamic imbalances. This paper gives attention to the reduction of the static and dynamic imbalance. Force/torque measurement system is used to measure the disturbance of the test reaction wheel. An identification method for the location and magnitude of the imbalance is suggested, and the corrections of the imbalance are performed using balancing method. Through balancing, the static and dynamic imbalance is remarkably reduced.
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spelling doaj.art-b37cf94256644f63bc452c225d0e86e82024-01-02T00:59:05ZengThe Korean Space Science SocietyJournal of Astronomy and Space Sciences2093-55872093-14092011-12-0128431131710.5140/JASS.2011.28.4.311Reaction Wheel Disturbance Reduction Method Using Disturbance Measurement TableDong-Ik Cheon0Eun-Jeong Jang1Hwa-Suk Oh2Department of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang 412-791, KoreaDepartment of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang 412-791, KoreaDepartment of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyang 412-791, KoreaMomentum changing actuators like reaction wheels and control moment gyros are generally used for spacecraft attitude control. This type of actuators produces force and torque disturbances. These disturbances must be reduced since they degrade the quality of spacecraft attitude control. Major disturbances are mainly due to static and dynamic imbalances. This paper gives attention to the reduction of the static and dynamic imbalance. Force/torque measurement system is used to measure the disturbance of the test reaction wheel. An identification method for the location and magnitude of the imbalance is suggested, and the corrections of the imbalance are performed using balancing method. Through balancing, the static and dynamic imbalance is remarkably reduced.http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2011/v28n4/OJOOBS_2011_v28n4_311.pdfreaction wheeldisturbancethree-dimensional measurement tableimbalancebalancing
spellingShingle Dong-Ik Cheon
Eun-Jeong Jang
Hwa-Suk Oh
Reaction Wheel Disturbance Reduction Method Using Disturbance Measurement Table
Journal of Astronomy and Space Sciences
reaction wheel
disturbance
three-dimensional measurement table
imbalance
balancing
title Reaction Wheel Disturbance Reduction Method Using Disturbance Measurement Table
title_full Reaction Wheel Disturbance Reduction Method Using Disturbance Measurement Table
title_fullStr Reaction Wheel Disturbance Reduction Method Using Disturbance Measurement Table
title_full_unstemmed Reaction Wheel Disturbance Reduction Method Using Disturbance Measurement Table
title_short Reaction Wheel Disturbance Reduction Method Using Disturbance Measurement Table
title_sort reaction wheel disturbance reduction method using disturbance measurement table
topic reaction wheel
disturbance
three-dimensional measurement table
imbalance
balancing
url http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2011/v28n4/OJOOBS_2011_v28n4_311.pdf
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