Zobrazeno 1 - 1
of 1
pro vyhledávání: '"Yakov G. Sapunkov"'
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
