Research on Rudder Travel Limit Function of Civil Aircraft Flight Control System

被引：0
|
作者：
Tang Zhishuai [1 ]
Hu Lingling [1 ]
机构：
[1] Shangai Aircraft Design & Res Inst, Shanghai 201210, Peoples R China
来源：
2022 34TH CHINESE CONTROL AND DECISION CONFERENCE, CCDC | 2022年
关键词：
Flight Control System; Rudder Travel Limit; Error Analysis;
D O I：
10.1109/CCDC55256.2022.10034339
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Safety is the basic feature of civil aircraft. In order to prevent catastrophic effect caused by rudder deflection beyond limit at high airspeed, most of the civil aircrafts generally provide the Rudder Travel Limit function. This thesis offers a new function architecture of Rudder Travel Limit, performs the error analysis and trade-off study, which frilly considers the impact of airspeed and actuator errors, can be used effectively in the Rudder Travel Limit function design of civil aircrafts.
引用
收藏
页码：406 / 411
页数：6
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