摘要
大气数据传感系统为飞行器飞行控制及投放初始状态给定与轨迹控制提供必要的静压、总压、迎角、侧滑角等参量,飞行器跨代发展诱发了大气数据传感系统参数解算基本要素获取方式由直接型演变为解耦提取。对大气数据传感系统构型形态和发展历程进行总结、提炼,系统分析了大气数据传感系统构型演变原因及过程、大气参数解算模型原理、故障大气参数诊断与检测流程、系统重构模型,总结了未来飞行器大气数据传感系统构型与参数解算设计重点研究方向。
The air data sensing system provides the necessary parameters for aircraft flight control,delivery and trajectory control,such as static pressure,total pressure,angle of attack,and sideslip angle.The inter-generation development of aircraft has induced the evolution of the basic element acquisition method for parameter calculation of air data sensing systems from direct type to decoupled extraction.This paper summarized and refined the configuration and development history of the air data sensing system and systematically analyzed the causes and processes of configuration evolution for the air data sensing system,the principle of air parameter calculation model,the diagnosis and detection process of fault air parameters,and system reconstruction model.It also summarized the key research directions for configuration and parameter solution design of air data sensing systems for aircraft in the future.
作者
熊亮
张睿
许斌
黄巧平
XIONG Liang;ZHANG Rui;XU Bin;HUANG Qiaoping(College of Automation,Northwestern Polytechnical University,Xi’an 710129,China;Department of Air Data System,Chengdu Caic Electronics Co.,Ltd.,Chengdu 610091,China)
出处
《北京航空航天大学学报》
北大核心
2025年第6期2004-2013,共10页
Journal of Beijing University of Aeronautics and Astronautics
