METHOD OF PRELAUNCHING ALIGNMENT OF HIGH-PRECISION MISSILES

摘要

FIELD: rocket engineering, topographic and geodetic referencing and guidance of high-precision missiles by signals of spacecraft. SUBSTANCE: main point of invention lies in usage of signals of system of navigational spacecraft for accurate location of high-precision missiles, for their orientation in space and for azimuthal guidance to target which is what is new. Realization of proposed method in missile complexes does not cause any principal difficulties as algorithm of computation process is rather simple. EFFECT: expanded capabilities of method of determination of coordinates of location with the aid of system of navigational spacecraft for prelaunch alignment of high-precision missiles, reduced time for preparation and launch of these missils.