Zobrazeno 1 - 2
of 2
pro vyhledávání: '"Alexei V. Molodenkov"'
Publikováno v:
Aerospace, Vol 10, Iss 5, p 402 (2023)
The problem of attitude optimal control of a spacecraft as a solid body with the energy spent on maneuvering a spacecraft taken as a quadratic functional, and a fixed transition time, is investigated. The dynamic configuration of a spacecraft and bou
Externí odkaz:
https://doaj.org/article/381986df726946228c4fff7ee6f0fcab
Autor:
Alexei V. Molodenkov, S. E. Perelyaev
Publikováno v:
Journal of Guidance, Control, and Dynamics. 44:1224-1228