Abstract
In this paper, the study of stabilization accuracy of a satellite equipped with a set of reaction wheels (RW) is presented. The model of motion takes into account possible static and dynamic reaction wheel imbalances. Due to the complexity of the model, which leads to the numerical issues, the effects of dynamic and static imbalances on inertial stabilization are studied analytically. As a result, estimations of the attitude and stabilization accuracy are presented in closed form.
Reference32 articles.
1. CubeWheel Small
https://www.cubesatshop.com/product/cubewheel-small/
2. CubeSat Reaction Wheels Control System SatBus 4RW0
https://nanoavionics.com/cubesat-components/cubesat-reaction-wheels-control-system-satbus-4rw/
3. Reaction Wheels Module
https://sputnix.ru/en/equipment/cubesat-devices/reaction-wheels-block
4. Reaction Wheels
http://www.sinclairinterplanetary.com/reaction-wheels
5. A Coupled Disturbance Analysis Method Using Dynamic Mass Measurement Techniques
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