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. ARP5007A has been reaffirmed to comply with the SAE five-year review policy.
Development Process - Aerospace Fly-By-Wire Actuation System
2020-10-09
Conference paper
English
Development Process - Aerospace Fly-By-Wire Actuation System
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