FIELD: aviation.
SUBSTANCE: this invention relates to the automation and can be used in aircraft automatic flight control systems Electrohydraulic follow-up drive comprises proportional-plus-derivative action controller and steering gear adjuster containing the first scaling amplifier, the first filter, the fifth amplifier with adjustable limitation, the second integrator, the second comparison element, the second differentiating element in limited frequency range, the second scaling amplifier, amplifier-summer with adjustable limitation and the second filter connected with each other and other assemblies of electrohydraulic follow-up device as stated in application documents.
EFFECT: drive sensitivity enhancement applicable to small signals with simultaneous control range extension and dynamic performance stabilisation under external load disturbance.
2 dwg
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Authors
Dates
2009-09-27—Published
2008-01-09—Filed