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pro vyhledávání: '"Mahboobeh Hossein Nejad"'
Publikováno v:
Measurement + Control, Vol 52 (2019)
The three-axis attitude tracking manoeuvre and vibration suppression of a flexible spacecraft in the presence of external disturbances are investigated in this paper. The spacecraft consists of a rigid hub and two flexible appendages. The Euler–Ber
Externí odkaz:
https://doaj.org/article/cad8c05e893b4d8fa6e6fd0d2ab3b3fc
Publikováno v:
Measurement + Control, Vol 52 (2019)
The three-axis attitude tracking manoeuvre and vibration suppression of a flexible spacecraft in the presence of external disturbances are investigated in this paper. The spacecraft consists of a rigid hub and two flexible appendages. The Euler–Ber