Economical digital attitude control of an information satellite at initial modes

Бесплатный доступ

We have presented algorithms for economical digital attitude control of an information satellite at initial modes - during its separation from launcher up to regular attitude stabilization in orbital reference frame. We also have represented the computer simulation results by the initial modes of orientation the satellite which is moving on sun-synchronous orbit.

An information satellite, attitude control, initial modes

Короткий адрес: https://sciup.org/148205271

IDR: 148205271

Статья научная