Reaction wheel configurations for high and middle inclination orbits
The purpose of this paper is to identify the low-power Reaction Wheel (RW) configuration for a 3-axis satellite attitude control at high and middle inclination orbits. All of the proposed RW configurations are evaluated through the numerical simulations with respect to an identical reference mission...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Asian Research Publishing Network
2015
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| Online Access: | http://psasir.upm.edu.my/id/eprint/46086/ http://psasir.upm.edu.my/id/eprint/46086/1/Reaction%20wheel%20configurations%20for%20high%20and%20middle%20inclination%20orbits.pdf |