Verification of attitude control system for a land-survey satellite by analysis of an image motion in onboard telescope
Abstract
Contemporary land-survey satellites are placed onto the orbit altitudes from 600 up to 1000 km. For such spacecraft we present elaborated methods for in-flight verification of its attitude control system by analysis of an image motion at optoelectronic converters' surface in focal plane of onboard telescope during a scanning imagery.
Published
2017-11-24
Section
Articles