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SAE ARP5007

Действует
Development Process - Aerospace Fly-By-Wire Actuation System
This document provides a description of a process for development of fly-by-wire actuation systems. Included are (1) the development of requirements for the servo-actuator hardware and the electronics hardware and software, (2) actuator and servo-electronics interface definitions and, (3) the required communications and interactions between the servo-actuator and the servo-electronics designers.
Тематика
Hydraulic control
Hydraulic drives
Parts
Tests and Testing
Electrohydraulics
Safety
Fly-by-wire control systems
Military aircraft
Hydraulic systems
Hydraulic motors
Unmanned aerial vehicles
Flight control systems
Fluid power systems
Fuel pumps
Hydraulic fittings
Flight control actuators
Sensors and actuators
Flight management systems
Hydraulic equipment
Hydraulic fluids