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

Leonid A. Igumnov; Vladimir S. Metrikin

doi:10.4028/www.scientific.net/AMM.775.314

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 775Effect of Correcting the Electro-Hydraulic Servo...

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

Abstract:

Response of a simplest servo system to an input perturbation is considered for two variants of correction of a servo drive to provide its stability and controllability. Numerical computations made it possible to find out the effect of the main parameters of the system on the dynamic characteristics of the controlling system.

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Periodical:

Applied Mechanics and Materials (Volume 775)

Pages:

314-318

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.775.314

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Online since:

July 2015

Authors:

Leonid A. Igumnov, Vladimir S. Metrikin

Keywords:

Electro-Hydraulic Controlling Systems, Mathematical Model, Rolling Systems, Stability

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References

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