M. R. Niknam

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

A long time ago, since the launch of the first artificial satellite in 1957, controling attitude of satellites has been considered by the designers and engineers of aerospace industry. Considering the importance of this issue various methods of control in response to this need have been presented and analyzed until now. In this paper, we propose and analyze a three-axis optimal control on the s...