Sliding Mode Attitude Control of Flexible Spacecraft with Rotational Components
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-6613-2_176
Reference27 articles.
1. George, V.I., Kamath, B.G., Thirunavukkarasu, I., et al.: Vibration control of flexible spacecraft using adaptive controller. Int. Adv. Sci. Eng. Inf. Technol. 2(1), 2088–5334 (2011). https://doi.org/10.18517/ijaseit.2.1.149
2. Wang, J., Li, D.X.: Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters, pp. 185–186. Springer, Singapore (2022). https://doi.org/10.1007/978-981-16-5097-0
3. Cui, M.Y., Xu, S.J., Jia, Y.H.: Flexible spacecraft attitude control based on perturbation method analysis. J. Beijing Univ. Aeronaut. Astronaut. 36(12), 1387–1391 (2010). https://doi.org/10.13700/j.bh.1001-5965.2010.12.003
4. Liu, M., Xu, S.J., Han, C.: Direct adaptive attitude tracking control of flexible spacecraft based on backstepping method. Acta Aeronautica et Astronautica Sinica 2034–2037 (2012)
5. Chen, Z.Y., Huang, J.: Attitude tracking and disturbance rejection of rigid spacecraft by adaptive control. IEEE Trans. Autom. Control 54(3), 600–605 (2009). https://doi.org/10.1109/TAC.2008.2008350
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