Control algorithms optimization at forming of the interacted effects in the balancing fuel transfer control system of the aircraft

The article represents the development of graph methods of analytical model building, which describes the control process dynamics. The forming of the interacted control is effected taking into account the existing status of the control and actuating elements with the time changes of the control system status. The information – measuring model of this class of the automatic control system is formed according to the revealed signs. Algorithms of effects forming according to the status of the control elements, which don’t characterize the system behavior unilaterally, are introduced in the control circuit according to the revealed signs.