DOI

Translated title of the contributionRigid body dynamics from the Euler equations to the spacecraft attitude control in the works of scientists from Saint Petersburg State University. Part 3
Original languageRussian
Pages (from-to)455-476
Number of pages22
JournalВЕСТНИК САНКТ-ПЕТЕРБУРГСКОГО УНИВЕРСИТЕТА. МАТЕМАТИКА. МЕХАНИКА. АСТРОНОМИЯ
Volume11(69)
Issue number3
DOIs
StatePublished - 2024

ID: 125869092