Nonlinear MPC for Attitude Guidance & Control of Autonomous Spacecraft
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Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-10047-5_2
Reference14 articles.
1. Stefanescu, M., Prioroc, C.: Automatic control systems for ESMO satellite using LQR control strategy. Adv. Astronaut. Sci. 145, 1571–1582 (2012)
2. Ofodile, I., Ehrpais, H., Slavinskis, A., Anbarjafari, G.: Stabilised LQR control and optimised spin rate control for nanosatellites. In: Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019, pp. 715–722 (2019)
3. Hegrenæs, Ø., Gravdahl, J.T., Tøndel, P.: Spacecraft attitude control using explicit model predictive control. Automatica 41, 2107–2114 (2005). https://doi.org/10.1016/j.automatica.2005.06.015
4. Yu, J., Zhang, Y., Jing, J.: Nonlinear MPC for attitude system of miniature satellite using multiple MEMS actuators. In: Proceedings of the World Congress on Intelligent Control and Automation (WCICA), pp. 2523–2528 (2012). https://doi.org/10.1109/WCICA.2012.6358298
5. Celani, F.: Robust three-axis attitude stabilization for inertial pointing spacecraft using magnetorquers (2014). https://doi.org/10.1016/j.actaastro.2014.11.027. arxiv:1411.2756
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