Three-axis optimal control of satellite attitude based on Ponteryagin maximum principle
Subject Areas : International Journal of Industrial Mathematics
M. R. Niknam
1
(
Department of Mathematics, Payame Noor University, P.O.Box 19395-3697, Tehran, Iran.
)
K. Kheiri
2
(
Faculty of Mathematical Sciences, University of Tabriz, Tabriz, Iran.
)
A. Heydari
3
(
Department of Mathematics, Payame Noor University, P.O.Box 19395-3697, Tehran, Iran.
)
Keywords:
Abstract :
