DEVELOPMENT OF AUTONOMOUS STRAPDOWN STELLAR-INERTIAL NAVIGATION SYSTEM
There is considered the main concept of creating airborne and ground-based stellar-inertial navigation systems (SINS), based on strapdown inertial navigation devices — stellar tracker, inertial navigation system and satellite navigation receiver. The requirements to optical and electronic components of inertial navigation system stellar tracker are formulated. The results of inertial navigation system model experimental processing both on ground and on the object are given. There are considered various astrocorrection versions of strapdown inertial navigation system implemented in stellar inertial navigation system