Three-axis optimal control of satellite attitude based on Ponteryagin maximum ‎principle‎

Subject Areas : International Journal of Industrial Mathematics

M. R. Niknam ¹ , K. Kheiri ² , A. Heydari ³

1 - Department of Mathematics, Payame Noor University, P.O.Box 19395-3697, Tehran, Iran.
2 - Faculty of Mathematical Sciences, University of Tabriz, Tabriz, Iran.
3 - Department of Mathematics, Payame Noor University, P.O.Box 19395-3697, Tehran, Iran.

Received: 2014-10-27 Accepted : 2014-10-27 Published : 2014-01-01

Keywords: