THE HIGH-ACCURACY GYROSCOPIC INSTRUMENTS FOR THE ATTITUDE CONTROL AND STABILIZATION SYSTEMS OF SPACECRAFTS AND ORBITAL SPACE STATIONS - THE EXPERIENCE IN DESIGN AND DEVELOPMENT

摘要

Aspects of developing of the high accuracy Strapdown Inertial Reference Unit (SIRU) intended for work in a control system by angular orientation of spacecrafts(SC) are considered. Design features of devices, design principles of gyroscope heat setting system and the precision electronic devices, the realized ways of achievement of raised reliability and a long lifetime are presented. The basic characteristics of devices are given. The estimation of results the SIRU using on spacecrafts of various purposes is given.