In-flight verification of attitude control system for a land-survey satellite at a final of its manufacturing ?

摘要

Contemporary land-survey satellites are placed in the orbits with altitude from of 600 up to of 1000 km. For such spacecraft at a final stage of its manufacturing we present developed methods for in-flight identification and verification of its attitude control system by analysis of an image motion in onboard telescope during a scanning optoelectronic imagery.