Hybrid adaptive sliding mode attitude control for earth pointing nanosatellites
Author:
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://link.springer.com/content/pdf/10.1007/s12567-023-00490-3.pdf
Reference29 articles.
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2. Chen, Y.H., Hong, Z.C., Lin, C.H., Chern, J.S.: Aerodynamic and gravity gradient stabilization for microsatellites. Acta Astronautica 46(7), 491–499 (2000). https://doi.org/10.1016/S0094-5765(99)00191-5
3. Nudehi, S.S., Farooq, U., Alasty, A., Issa, J.: Satellite attitude control using three reaction wheels. Proceedings of the American Control Conference pp. 4850–4855 (2008). https://doi.org/10.1109/ACC.2008.4587262
4. Manggala, F.H., Ramadhan, R.P., Wijanto, H., Mayditia, H., Edwar, E., Vidyaningtyas, H.: rototype of Micro Reaction Wheel for Cubesat. TSSA 2019 - 13th International Conference on Telecommunication Systems, Services, and Applications, Proceedings pp. 209–213 (2019). https://doi.org/10.1109/TSSA48701.2019.8985474
5. Hsiao, D.C., Hsieh, M.F.: Integrated Design and Analysis of Reaction Wheel Motor Applied to Satellite Attitude Control. ICEMS 2021 - 2021 24th International Conference on Electrical Machines and Systems pp. 1090–1094 (2021). https://doi.org/10.23919/ICEMS52562.2021.9634235
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