Procedure for forming nominal control program of solar sail spacecraft heliocentric movement using locally optimal control laws

The paper is devoted to the non-coplanar interplanetary flight Earth-Venus of the spacecraft equipped with a solar sail. The goal of the heliocentric movement is to transfer a spacecraft with a non-perfectly reflecting solar sail into the Hill’s sphere of the Venus with zero hyperbolic excess speed....

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Bibliographic Details
Main Author: R. M. Khabibullin
Format: Article
Language:Russian
Published: Association «Technology Platform «National Information Satellite System» 2020-03-01
Series:Космические аппараты и технологии
Subjects:
Online Access:http://journal-niss.ru/downloads.php?vol_all=31&paper_num=1