DOI

The article considers the strategy of keeping the spacecraft in the vicinity of the unstable Lagrange point (libration point) of the Sun — Earth system. This strategy involves the use of special management. This control acts collinearly to the Sun — Earth line and ensures Lyapunov stability of the orbital motion. The implementation of such control is proposed using a solar sail. The advantages and difficulties of such a strategy are discussed.
Translated title of the contributionControlling the orbital motion of the spacecraft near the libration point by changing the solar sail reflectivity
Original languageRussian
Pages (from-to)298-306
Number of pages9
Journal ВЕСТНИК САНКТ-ПЕТЕРБУРГСКОГО УНИВЕРСИТЕТА. ПРИКЛАДНАЯ МАТЕМАТИКА. ИНФОРМАТИКА. ПРОЦЕССЫ УПРАВЛЕНИЯ
Volume20
Issue number2
DOIs
StatePublished - 8 Jul 2024

ID: 122804409