Influence of errors of azimuth exposure of inertial navigational systems (INS) is analysed on exactness of position-finding vertical line, absolute speed of flight and passed way. As a method of determination of course after an induction sensor differs a most operationability and this sensor is the unique for the exposure of course in flight, the task of increase of exactness of magnetic channel INS is put.
inertial navigational system, azimuth exposure, induction sensor
"Vplyv pokhybok azymutalnoho vystavlennia inertsialnykh navihatsiinykh system na tochnist vyznachennia navihatsiinykh parametriv" ,
Scientific Works of Kharkiv National Air Force University,