飞行器飞行大气数据传感技术发展现状与展望  

Development status and prospects of flight air data sensing technology for aircraft

作　　者：熊亮[1,2] 张睿 龙彦志[2] XIONG Liang;ZHANG Rui;LONG Yanzhi(College of Automation,Northwestern Polytechnical University,Xi'an 710129,China;Department of Air Data System,Chengdu CAIC Electronics Co.LTD,Chengdu 610091,China)

机构地区：[1]西北工业大学自动化学院,西安710129 [2]成都凯天电子股份有限公司大气数据系统研究室,成都610091

出　　处：《航空学报》2024年第5期202-217,共16页Acta Aeronautica et Astronautica Sinica

基　　金：国家级项目。

摘　　要：飞行器飞行大气数据传感技术是现代飞行器全包线飞行控制、通信导航和武器打击轨迹精确控制获取飞行大气参数测量的关键或重要途径。回顾了飞行器飞行大气数据传感技术发展历程,阐述了技术跨代发展的驱动因素和系统架构设计、压力受感与传递转换、参数解算模型设计、复杂气象环境适应性设计、系统校准与飞行验证五项关键技术解决情况,分析了现有技术的不足与缺陷,从现代飞行器发展与应用需要出发,结合工程技术研究成果,提出了飞行器飞行大气数据传感技术未来重点发展方向。The flight air data sensing technology is a key or important approach to obtaining flight air parameters for full envelope flight control,communication navigation and weapon strike trajectory of modern aircraft.This paper reviews the development history of air data sensing technology for aircraft,elaborates on the driving factors and system architecture design for cross-generation development of technology and the development of five key technologies,including system architecture design,pressure sensing and transfer conversion,parameter solution model design,complex meteorological environment adaptability design,and system calibration and flight verification.The deficiencies and defects of current technologies are analyzed.According to the development and application needs of modern aircraft,the future development direction of flight air data sensing technology for aircraft is proposed based on research results in engineeringpractice.

关 键 词：大气数据系统 大气参数测量 大气参数解算 压力受感技术 气象环境适应性 

分 类 号：V247.16[航空宇航科学与技术—飞行器设计]