FIELD: physics.
SUBSTANCE: system has comprises a sensor unit, a processor and an actuating mechanism connected in series. The system also has ultrasonic and/or radio frequency locators, whose outputs are connected to the second input of the processor through a controlled delay unit. The second output of the sensor unit is connected to the control input of the controlled delay unit.
EFFECT: higher margin of stability of the stabilisation system of subsonic aircraft in a difficult, fast-changing aerodynamic environment during flight and when landing.
2 dwg
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