An iteration method of optimal control synthesis for space vehicle reorientation based on an algorithm with a prediction model

An algorithm for the synthesis of the optimal control of space vehicle reorientation is developed on the basis of a prediction model. The use of an additive programmed component in the algorithm, obtained at the preliminary stage of the synthesis procedure, makes it possible to significantly improve the quality of control and extend the available length of the control generation cycle. The iteration synthesis method proposed here can also be used at the stage of the real-time operation of the system.