1.u0430u043du0442u0435u043du043du0430u00a0 system with stabilized plane u0432u0440u0430u0449u0435u043du0438u00a0 review the ship's radar, u0438u043cu0435u044eu0449u0430u00a0 connecting u043fu043eu0434u0432u0435u0441 and caps, u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0 because antennas gear system u0432u044bu043fu043eu043bu043du00a0u044eu0442 as symmetrical, balanced center of mass gyroscope, which handles most u043du0430u0445u043eu0434u0438u0442u0441u00a0 in the centre of symmetry.with the u0430u043du0442u0435u043du043du0430u00a0 system has u0433u0438u0440u043eu0441u043au043eu043fu0438u0447u0435u0441u043au0438u043c effect by the kinetic moment u0432u0440u0430u0449u0435u043du0438u00a0 system.;2. u0430u043du0442u0435u043du043du0430u00a0 system 1, u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0, as an executive element of the correction plane u0432u0440u0430u0449u0435u043du0438u00a0 use u0441u043eu043bu0435u043du043eu0438u0434u044b the impulse force, and to quality of information of correction is zero - drift angular velocity sensors and laser sensors antenna system.;3. u0430u043du0442u0435u043du043du0430u00a0 system 1, u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0, cap tightly u0441u0432u00a0u0437u0430u043d with antenna system and u0432u0440u0430u0449u0430u0435u0442u0441u00a0 together with her.
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