论文部分内容阅读
电传操纵系统已经成为民用运输类飞机操纵系统的主流。现行适航规章与操稳特性相关的要求主要是基于机械操纵飞机制定的,而电传操纵系统可以设计成与机械操纵不同的操纵性和稳定性,使得适航规章要求与电传操纵飞机之间存在不一致。对波音和空客公司的电传操纵系统操稳设计特征进行了分析,对与适航性密切相关的几个关键问题进行了对比研究,包括主操纵装置型式、响应类型、稳定性特征、大迎角保护、操纵品质评价以及飞行控制律需求捕获与确认等问题,为电传操纵运输机的设计与适航审定提供了借鉴。
Fly-by-wire system has become the mainstream of civil transport aircraft control system. The current requirements for airworthiness regulation and handling characteristics are mainly based on mechanically controlled aircraft, which can be designed to operate and stabilize differently than mechanical controls, making airworthiness regulations and telex-controlled aircraft Inconsistent between. Based on the analysis of the stability design characteristics of the telemanipulation system of Boeing and Airbus, several key issues closely related to airworthiness were studied, including the type of main control device, the type of response, the stability characteristics, the large Angle of attack protection, control quality evaluation and flight control law requirements capture and validation and other issues, provide a reference for the design and airworthiness validation of the telemodal transport aircraft.