FIELD: gyro-navigation instrumentation engineering. SUBSTANCE: output parameters are produced in response to the signals of accelerometers and roll-angle and pitch-angle pick-offs of at least two gyroplatforms, in a two-axis gimbal mount with a three-frame gyro each; control signals of the gyros are preset so as to ensure a different value of speed error at each stabilized gyroplatform and at the same time eliminate ballistic deviations. The gyroplatform speed error behavior law is preset proceeding from the minimum influence of instrument errors on the accuracy of generation of output parameters. EFFECT: simplified implementation of method at enhanced accuracy. 1 dwg
