FIELD: transport.
SUBSTANCE: invention relates to aerostatics. Control over airship including airframe, tail unit, nacelle with payload and onboard systems and differs in that airship required stability and controllability at takeoff, flight and landing result from application of gyro rotor with controlled vector of the full aerodynamic force. Gyro rotor (1) can incline relative to lengthwise and crosswise directions with separate sustainer power plants that perform their traction functions irrespective gyro rotor.
EFFECT: simplified control.
1 dwg
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