航天器环境工程
航天器環境工程
항천기배경공정
SPACECRAFT ENVIRONMENT ENGINEERING
2015年
1期
89-94
,共6页
张鹏%任春珍%尚明友%沈锋钢
張鵬%任春珍%尚明友%瀋鋒鋼
장붕%임춘진%상명우%침봉강
环境差异%重力环境%压力环境%安装精度%结构变形
環境差異%重力環境%壓力環境%安裝精度%結構變形
배경차이%중력배경%압력배경%안장정도%결구변형
environmental differences%gravity environment%pressure environment%installation precision%structure deformation
文章分析了地面重力环境和在轨内压环境对不同位置和状态下的载人航天器陀螺组件及姿轨控敏感器设备安装精度的影响,并进行了试验验证,分析结果与试验数据一致性较好。研究结果显示:设备布局位置不同,其安装精度受环境差异的影响程度也不同;航天器在空载、垂直停放状态下,设备安装精度受地面重力环境影响较小;陀螺组件和姿轨控敏感器A的安装精度受在轨内压环境影响较小,在地面常压环境下的精测结果能够真实反映其在轨状态,而姿轨控敏感器B的安装精度受压力环境影响明显。以上结果可为航天器设备布局及精度测量工作提供借鉴。
文章分析瞭地麵重力環境和在軌內壓環境對不同位置和狀態下的載人航天器陀螺組件及姿軌控敏感器設備安裝精度的影響,併進行瞭試驗驗證,分析結果與試驗數據一緻性較好。研究結果顯示:設備佈跼位置不同,其安裝精度受環境差異的影響程度也不同;航天器在空載、垂直停放狀態下,設備安裝精度受地麵重力環境影響較小;陀螺組件和姿軌控敏感器A的安裝精度受在軌內壓環境影響較小,在地麵常壓環境下的精測結果能夠真實反映其在軌狀態,而姿軌控敏感器B的安裝精度受壓力環境影響明顯。以上結果可為航天器設備佈跼及精度測量工作提供藉鑒。
문장분석료지면중력배경화재궤내압배경대불동위치화상태하적재인항천기타라조건급자궤공민감기설비안장정도적영향,병진행료시험험증,분석결과여시험수거일치성교호。연구결과현시:설비포국위치불동,기안장정도수배경차이적영향정도야불동;항천기재공재、수직정방상태하,설비안장정도수지면중력배경영향교소;타라조건화자궤공민감기A적안장정도수재궤내압배경영향교소,재지면상압배경하적정측결과능구진실반영기재궤상태,이자궤공민감기B적안장정도수압력배경영향명현。이상결과가위항천기설비포국급정도측량공작제공차감。
This paper analyzes the influence of the ground gravity environment and the space pressure environment on the installation precision of the gyro assembly and the attitude-control and orbit-control sensors of manned spacecraft at different positions and in different states. The verification test shows that the analysis results are consistent with the experimental data. It is shown that the influence of the environmental differences on the equipment installation precision differs when the layout of equipment is different. Under the conditions of the no-load and the vertical parking conditions, the ground gravity environment has little effect on the installation precision of equipment. The installation precisions of the gyro assembly and the attitude-control and orbit-control sensor A are little affected by the space pressure environment, and the precision measurement results in the ground atmospheric environment can reflect the state of equipment on orbit, while the installation precisions of the attitude-control and orbit-control sensor B are obviously affected by the space pressure environment. The research may provide a reference for the layout and the precision measurement of spacecraft equipment.