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Primary Flight Control Hydraulic Actuation System Interface Definition

A-6A3 Flight Control and Vehicle Management Systems Cmt

出版	SAE International, 2015
URL	http://books.google.com.hk/books?id=eLTbzwEACAAJ&hl=&source=gbs_api

註釋

This SAE Aerospace Information Report (AIR) provides a description of the interfaces and their requirements for generic and specific hydraulic actuation systems used in the flight control systems of manned aircraft. Included are the basic control system characteristics and functional requirements, and the essential interfaces (structural, mechanical, hydraulic power, control input, status monitoring, and environment). Major design issues, requirements, and other considerations are presented and discussed. This document contains information addressing aspects of technology that are not currently undergoing substantial development.