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On the Effect of Correcting the Electro-Hydraulic Servo Drive on the Stability and Controllability of an Aircraft

Vladimir Metrikin, Michael Peysel, Leonid Igumnov
Response of the simplest servo system to an input perturbation is considered for two variants of correction of the servo drive to provide solutions for its stability and controllability. Numerical computations are employed to study the effect of the system’s main parameters on the dynamic characteristics of an aircraft.
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