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Advanced Flight Control Actuation Systems and Their Interface with Digital Commands
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English
Abstract
Advanced flight control actuation systems require that the actuator be capable of interfacing with centralised digital computing systems.
The actuation specialist must consider the electro hydraulic system as a whole, including the closed loop servo electronics, from the command distribution databus to the final output member.
This paper discusses the overall approach of a primary flight control specialist company, with the lateral implications of direct drive and multi redundant valve configurations, higher system pressures and direct rotary actuation.
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