Pulse-width control of satellite during initial stop of its rotation and a station-keeping on sun-synchronous orbit
Abstract
We consider an information satellite which may be placed on an orbit with altitude from 600 up to 1000 km. We study problems on economical control of eight electro-reaction engines for initial stop of the spacecraft rotation and its station-keeping on sun-synchronous orbit.
Published
2017-02-28
Section
Articles