FIELD: physics; aviation.
SUBSTANCE: invention relates to experimental aerodynamics of aircraft and can be used in analysis of characteristics of aerodynamic model (ADM) during testing in wind tunnel. Method includes supply of control signal to control device of steering surface drive with subsequent generation of output signal for drive, movement of its rod and deviation of steering surface, at that, required angle of inclination of steering surface is set, signal is received on current state of inclination of steering surface, control signal is supplied to control device of steering surface actuator simultaneously with supply of signal on current state of steering surface to it, and generation of output signal for drive is performed by summation of signals received by control device of steering surface drive.
EFFECT: technical result consists in possibility to reduce time of pipe experiment.
1 cl, 5 dwg
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| HINGE MOMENT OF THE REJECTED SURFACE MEASUREMENT DEVICE | 2018 |
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