航空工程进展2025，Vol.16Issue(3)：82-89,8.DOI:10.16615/j.cnki.1674-8190.2025.03.08
基于侧滑角估算的飞机迎角信号修正技术研究
Study on correction technology of aircraft angle-of-attack signal based on estimation of side-slip angle
薛源 1刘世民 1魏剑龙1
作者信息
- 1. 中航工业第一飞机设计研究院 飞控系统设计研究所,西安 710089
- 折叠
摘要
Abstract
The angle-of-attack signal is very important for modern fly-by-wire flight control system aircraft.The inconsistency of the local airflow on both sides of the nose will cause the difference of the angle-of-attack signal.The signal-monitoring voting logic of the flight control system will judge the angle-of-attack signal and make the angle-of-attack availability decrease.By studying the relationship between the lateral overload and the side-slip an-gle,the side-slip angle is estimated by the lateral overload,the angle-of-attack signal correction method based on the side-slip angle estimation and the complete monitoring voting algorithm is established to improve the availabili-ty of the angle-of-attack signal under the condition of large side-slip.The simulation results show that the proposed method is successful in estimating the side-slip angle,and the angle-of-attack signal on both sides of the nose is consistent with the modified side-slip angle,which solves the problem of over-error of the angle-of-attack signal caused by the large side-slip state and has good correction effect.关键词
迎角修正/侧滑角估算/监控表决/大侧滑/飞行控制系统Key words
angle-of-attack correction/side-slip angle estimation/monitoring voting/large side-slip/flight con-trol system引用本文复制引用
薛源,刘世民,魏剑龙..基于侧滑角估算的飞机迎角信号修正技术研究[J].航空工程进展,2025,16(3):82-89,8.
