id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
ejpam-2135	Zarina, Samigulina Ildusovna; Olga, Shiryeva Ivanovna; Galina, Samigulina Ahmetovna; Hassen, Fourati Ben Mahmoud	Robust control system for Spacecraft Motion Trajectory	2014	15	.pdf	application/pdf	6153	292	59	Then, the problem of model reference adaptive control system can be seen as a regulation problem for the spacecraft system displaced from its equilibrium state (defined by AM = AS , BM = BS) using the adjusted parameters fA and fB (see Figure 1). Optimal Mathematical Model of SMT Let consider the mathematical model of SMT which is described by the nonlinear differen- tial equations system based on the boundary conditions [7]:      ṗ (t) = 2 � p (t) �(3/2) (Q (t) + 1)−1 aφ Q̇ (t) = � −p (t) �(−3/2) (Q (t) +	cache/ejpam-2135.pdf	txt/ejpam-2135.txt