Analysis of optic gyroscope features, affecting instrument reliability during its operation

In hired it was verification of optical gyroscopes by development of stand on the basis of effect of Sаnyaка for verification of optical gyroscopes of the inertial system IRS airplane of "Boeing" in the conditions of Airline of "Uzbekistan airways techniсs"( Airline "UAT"). Within the framework of hired формулирована there is the detailed model of verification of optical gyroscope, allowing to educe the degree of his vulnerability, the base criterion of work is stopped up in basis of that - refuse.