Reliable attitude control integrating reaction wheels and embedded asymmetric magnetorquers for detumbling CubeSats
Author:
Funder
European Space Agency
Netherlands Space Office
Publisher
Elsevier BV
Reference33 articles.
1. Optimized design of embedded air coil for small satellites with various dimensions;Ahmed Khan;J. Aerosp. Inf. Syst. Doi,2021
2. Active attitude control for microspacecraft; a survey and new embedded designs;Ahmed Khan;Adv. Space Res.,2022
3. CubeSats detumbling using only embedded asymmetric magnetorquers;Ahmed Khan;Adv. Space Res.,2023
4. Design, implementation, and thermal modeling of embedded reconfigurable magnetorquer system for nanosatellites;Ali;IEEE Trans. Aerosp. Electron. Syst.,2015
5. Design & thermal modeling of solar panel module with embedded reconfigurable Air-Coil for micro-satellites;Ali;PLoS One,2018
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