Reaction Wheel Disturbance Reduction Method Using Disturbance Measurement Table

Details Reaction Wheel Disturbance Reduction Method Using Disturbance Measurement Table Reaction Wheel Disturbance Reduction Method Using Disturbance Measurement Table

Dec 2011

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2011jass...28..311c&link_type=abstract

Journal of Astronomy and Space Sciences. Vol. 28, no. 4, 311-317

Astronomy and Astrophysics

Astronomy

Reaction Wheel, Disturbance, Three-Dimensional Measurement Table, Mbalance, Balancing

Scientific paper

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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