Analysis of residual gas disturbance on the inner satellite of Inner Formation Flying System  

作　　者：GU ZhenFeng WANG ZhaoKui ZHANG YuLin 

机构地区：[1]School of Aerospace,Tsinghua University,Beijing 100084,China

出　　处：《Science China(Technological Sciences)》2012年第9期2511-2517,共7页中国科学（技术科学英文版）

基　　金：supported by the National Natural Science Foundation of China (Grant No. 11002076)

摘　　要：The Inner Formation Flying System （IFFS） consisting of an freely flying in the shield cavity can construct a pure gravity outer satellite and an inner satellite which is a sphere proof mass orbit to precisely detect the earth gravity field. The residual gas in the cavity is a significant disturbance source due to the temperature inhomogeneity and relative motion of the inner satellite. The expressions of the disturbance forces were derived based on the property of rarefied gas, including the radiometer effect and the damping force. According to the current design of IFFS, heat transfer analysis of the cavity and the inner satellite was carried out, and the surface temperature distribution of the cavity and the inner satellite was given. The relative motion of the inner satellite was obtained from the formation control simulation of IFFS. Then the residual gas disturbance was calculated. The disturbance acceleration acting on the inner satellite due to the radiometer effect was on the order of 10^-11 m s^-2 and the damping acceleration was on the order of 10^-15 m s^-2.

关 键 词：Inner Formation Flying System inner satellite residual gas radiometer effect residual gas damping 

分 类 号：U463.5[机械工程—车辆工程] TN927.2[交通运输工程—载运工具运用工程]