航天器环境工程2024，Vol.41Issue(3)：277-282,6.DOI:10.12126/see.2023059
卫星主动段力学环境监测系统设计
Design of mechanical environmental monitoring system for satellite powered-flight phase
摘要
Abstract
To obtain the acceleration and force of satellite-rocket interface for satellite powered-flight phase accurately,a mechanical environmental monitoring system was designed.The system is composed of vibration monitoring unit,vibration sensors and strain gauges.The vibration monitoring unit was with three operating modes:powered-flight phase measurement mode,on-orbit vibration data analysis mode,and vibration data transmission mode.It adopts strain-based dynamic load identification technology on the satellite-rocket interface,enabling data acquisition from 6 channels of vibration mechanical sensors and 24 channels of strain data.The ground test shows that the vibration measurement accuracy of the system reaches 10%,and the maximum error between the strain measurement and the strain data collected by the LMS(LabVIEW Measurement Studio)system is less than 4%.The measurement results of the mechanical environment of the powered-flight phase on board may provide a reference for optimizing the satellite analysis model and improving the simulation conditions for the satellite ground mechanical environment,and provide important technical support for the subsequent development and application of satellites.关键词
卫星主动段/星箭连接环/力学环境/力学传感器/振动测量/应变测量Key words
satellite powered-flight phase/satellite-rocket connection ring/mechanical environment/mechanical sensor/vibration measurement/strain measurement分类
航空航天引用本文复制引用
孙延博,贾奥男,虞自飞,方厚招,顾桂华..卫星主动段力学环境监测系统设计[J].航天器环境工程,2024,41(3):277-282,6.基金项目
国家重点研发计划项目(编号:2019YFA0708904) （编号:2019YFA0708904）
