FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering and may be used in developing helicopters with in-line rotors. Proposed system comprises set of transmitters, analysis unit and set of receivers. Receiver outputs are connected to first set of data inputs of analysis unit. Analysis unit output is connected via onboard computer with helicopter control and/or indication components. Second set of data inputs s connected with appropriate set of onboard computer outputs.
EFFECT: helicopter safety.
3 cl, 3 dwg
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