Muhammad R. Methodic of initial azimuth orientation and correction of inertial navigation system of flying object

In the result of completion of dissertation work achieved new results: first on the bases of fundamental position of analysis, synthesis, optimization formed, based, researched scientific-technical problems to enhance and check accuracy of prospective combined OASAO inertial navigation system of flying object; designed and developed methodic and optical with feed back double channel servo system of initial azimuth orientation (INS FO); first derived and developed methodic and device for checking given optical with feed back servo system for the positioning of INS FO, in addition, modernized theoretical position and methodology of marking effectiveness of apparatus complex of optical with feed back servo system of initial azimuth orientation of INS FO.