Satellite attitude guidance and economical digital control during initial modes

  • Tatyana Somova

Abstract

We present algorithms for attitude guidance and economical digital control of an information satellite at initial modes during from its separation from a launcher rocket up to its regular attitude stabilization in orbital reference frame. We represent the computer simulation results on the initial orientation modes of a land-survey satellite in sun-synchronous orbit.

Published
Aug 25, 2018
How to Cite
SOMOVA, Tatyana. Satellite attitude guidance and economical digital control during initial modes. Journal | MESA, [S.l.], v. 9, n. 3, p. 365-372, aug. 2018. Available at: <http://nonlinearstudies.com/index.php/mesa/article/view/1749>. Date accessed: 20 oct. 2018.