In order to detect potential faults of the redundant fly-by-wire flight control system in advance,BIT technology is commonly adopted in third and fourth generation aircraft to test the integrity of components of flight control system before flight.This article analyzes the content,design methods,and various factors that affecting the design threshold of flight control system BIT testing,and proposes corresponding PBIT testing optimization strategies.
关键词
飞控系统架构/PBIT/复杂环境/虚警率/伺服测试
Key words
Flight control system architecture/PBIT/Complex environment/False alarm rate/Servo testing