IMPROVING THE ACCURACY OF THE CONTROL ALGORITHM OF ANGULAR ORIENTATION THE SPACECRAFT
The article suggested technical solution, providing autonomous high-precision navigation and control of the spacecraft (SC) on geostationary orbit. The solution is based on a mathematical model of motion the SC with a star tracker which takes into account data from the angular rate sensors. The mathematical model and algorithm of the control system are shown. Proposed the cyclogram of work the integrated spacecraft control system taking into account errors of the estimates of the angular orientation.