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pro vyhledávání: '"Valiollah Shahbahrami"'
Publikováno v:
فصلنامه علوم و فناوری فضایی, Vol 16, Iss 4, Pp 1-13 (2021)
In this paper, a robust adaptive hybrid control approach based on a combination of super-twisting and non-singular terminal sliding mode control (STNSMC) approaches for vibration and attitude control of a flexible spacecraft with fully coupled dynami
Externí odkaz:
https://doaj.org/article/41a25a35f7564603b4b3a4c9f26f928e