Model complex for analysis and synthesis of spacecraft motion control system on active journey legs

The problems are considered connected with developing the complex of mathematical models for the spacecraft motion control system elements on the active journey legs with allowance for the constructive realization peculiarities. The models are obtained on the basis of three key moments: a priori information; deductive and inductive approaches; hierarchy. The general and specific model modifications are developed for the angular stabilization operating mode. Experimental revision of the obtained models is performed by numerical modeling in the problem-oriented medium. Comparative results are given.