Optimum Design of Robust Adaptive Controller with Actuator Constraints
Author:
Publisher
Springer Science and Business Media LLC
Subject
Computer Science Applications,Control and Systems Engineering
Link
https://link.springer.com/content/pdf/10.1007/s12555-019-0356-2.pdf
Reference24 articles.
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2. M. Navabi and M. Barati, “Mathematical modeling and simulation of the earth’s magnetic field: a comparative study of the models on the spacecraft attitude control application,” Applied Mathematical Modelling, vol. 46, pp. 365–381, 2017.
3. M. Navabi, A. Davoodi, and M. Reyhanoglu, “Modeling and control of a nonlinear coupled spacecraft-fuel system,” Acta Astronautica, vol. 162, pp. 436–446, 2019.
4. M. Navabi, A. Davoodi, and M. Reyhanoglu, “Optimum fuzzy sliding mode control of fuel sloshing in a spacecraft using PSO algorithm,” Acta Astronautica, vol. 167, pp. 331–342, 2020.
5. M. Navabi and M. R. Hosseini, “Spacecraft quaternion based attitude input-output feedback linearization control using reaction wheels,” Proc. of the 8th International Conference on Recent Advances in Space Technologies, IEEE, pp. 97–103, 2017.
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