BASIC PRINCIPLES OF CONSTRUCTION OF THE LAUNCHER «SOYUZ-2» INTEGRATED NAVIGATION CONTROL SYSTEM

摘要

The basic principles of the construction of the integrated navigation control system are considered. These principles are determined and realized with deep structural and hardware modernization of the launcher «Soyuz-2». The results of full-scale tests and data of considerably new characteristics of the updated control system are given. These data are received both for the prelaunch planning stage and for the launcher flight leg on the basis of a wide implementation of digital systems.