静电加速度计对重力卫星平台的要求分析
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摘要
静电加速度计是重力卫星的核心有效载荷,其非保守力测量精度是地球重力场反演任务成功执行的有效保证。文章分析了静电加速度计的测量信号以及对重力卫星平台的指标要求,重点指出满足这些要求应解决的关键技术,最后建议我国开展重力卫星研究。
Electrostatic accelerometer is a key payload for gravity satellite,used for measuring the non-gravitational acceleration.Its detection accuracy eventually determines the success of the Earth's gravity recovery mission.This paper discusses the observation signal of electrostatic accelerometer and its requirements on gravity satellite platform.Related key technologies are addressed.The significance of gravity satellite for our country is analyzed.
Electrostatic accelerometer is a key payload for gravity satellite,used for measuring the non-gravitational acceleration.Its detection accuracy eventually determines the success of the Earth's gravity recovery mission.This paper discusses the observation signal of electrostatic accelerometer and its requirements on gravity satellite platform.Related key technologies are addressed.The significance of gravity satellite for our country is analyzed.
引文
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[10]Kang Z,Tapley B,Bettadpur S,et al.Precise orbit determination for GRACE using accelerometer data[J].Advance in Space Research,2006,38(9):2131-2136
[11]宋仁旺,陈琳英.静电悬浮加速度计关键技术剖析[J].计算机工程与应用,2009,45(34):67-73
[12]彭承明,曾占魁,舒嵘,等.静电加速度计标度因数和零偏误差标定[J].中国惯性技术学报,2009,17(5):582-585
[13]陈光锋,唐富荣,薛大同.重力卫星在轨质心修正原理[J].宇航学报,2005,26(5):567-570
[14]薛大同.非重力加速度测量对重力测量卫星的要求[C]//中国宇航学会飞行器总体专业委员会2006年学术研讨会,2006:121-125
[15]Stanton R H,Bettadpur S,Dunn C E,et al.Science&mission requirements document[R].Jet propulsion laboratory,University of Texas Center for Space Research,GEO Forschung Zentrum Potsdam,1998
[16]Furun W.Study on center of mass calibration and K-band ranging system calibration of GRACE mission[D].Ph D Dissertation,Austin,University of Texas at Austin,2000
[17]徐寿岩,唐军,李文滋,等.体装组合板式小卫星太阳电池阵的设计[J].电源技术,1997,21(6):235-237
[18]Davis E S,Dunn C E,Stanton R H,et al.The GRACE mission:meeting the technical challenges[R].California Institute of Technology,1999
[19]Folkner W M,Vine G D,Klips W M.Laser frequency stabilization for GRACE-II[R].California Institute of Technology,2010
[20]Herman J,Presti D,Codazzi A,et al.Attitude control for GRACE[C]//Proceedings of the 18th International Symposium on Space Flight Dynamics,Munich,2004
[21]Furun W,Srinivas B,Himanshu S.Determination of center-of-mass of gravity recovery and climate experiment satellites[J].Journal of Spacecraft and Rockets,2010,47(2):371-379
[22]廖鹤,赵艳彬,孙克新,等.质量特性调整机构在航天器中的应用[J].航天器环境工程,2009,26(2):168-171
[2]Kim J R.Simulation study of a low-low satellite to satellite tracking mission[D].Ph D Dissertation,Austin,University of Texas at Austin,2000
[3]Klees R,Koop R,Visser P,et al.Efficient gravity field recovery from GOCE gravity gradient observations[J].Journal of Geodesy,2000,74(7):561-571
[4]周泽兵,白彦峥,祝竺,等.卫星重力测量中加速度计在轨参数校准方法研究[J].中国空间科学技术,2009,29(6):74-80
[5]Gerlach C,Sneeuw N,Jeongrae K,et al.CHAMP gravityfield recovery using the energy balance approach[J].Advancein Geosciences,2003(1):73-80
[6]Tapley B,Ries J,Bettadpur S,et al.GGM02—an improved Earth gravity field model from GRACE[J].Journal of Geodesy,2000,79(8):467-478
[7]Enrico C,Luca M.All-propulsion design of the drag-free and attitude control of the European satellite GOCE[J].Acta Astronautica,2009,64(2):325-344
[8]Klokoník J,Wagner C A,Kostelecky J,et al.Variations in the accuracy of gravity recovery due to ground track variability:GRACE,CHAMP,and GOCE[J].Journal of Geodesy,2008,82(12):917-927
[9]Bruinsma S L,Forbes J M.Properties of traveling atmospheric disturbances inferred from CHAMP accelerometer observations[J].Advances in Space Research,2009,43(3):369-376
[10]Kang Z,Tapley B,Bettadpur S,et al.Precise orbit determination for GRACE using accelerometer data[J].Advance in Space Research,2006,38(9):2131-2136
[11]宋仁旺,陈琳英.静电悬浮加速度计关键技术剖析[J].计算机工程与应用,2009,45(34):67-73
[12]彭承明,曾占魁,舒嵘,等.静电加速度计标度因数和零偏误差标定[J].中国惯性技术学报,2009,17(5):582-585
[13]陈光锋,唐富荣,薛大同.重力卫星在轨质心修正原理[J].宇航学报,2005,26(5):567-570
[14]薛大同.非重力加速度测量对重力测量卫星的要求[C]//中国宇航学会飞行器总体专业委员会2006年学术研讨会,2006:121-125
[15]Stanton R H,Bettadpur S,Dunn C E,et al.Science&mission requirements document[R].Jet propulsion laboratory,University of Texas Center for Space Research,GEO Forschung Zentrum Potsdam,1998
[16]Furun W.Study on center of mass calibration and K-band ranging system calibration of GRACE mission[D].Ph D Dissertation,Austin,University of Texas at Austin,2000
[17]徐寿岩,唐军,李文滋,等.体装组合板式小卫星太阳电池阵的设计[J].电源技术,1997,21(6):235-237
[18]Davis E S,Dunn C E,Stanton R H,et al.The GRACE mission:meeting the technical challenges[R].California Institute of Technology,1999
[19]Folkner W M,Vine G D,Klips W M.Laser frequency stabilization for GRACE-II[R].California Institute of Technology,2010
[20]Herman J,Presti D,Codazzi A,et al.Attitude control for GRACE[C]//Proceedings of the 18th International Symposium on Space Flight Dynamics,Munich,2004
[21]Furun W,Srinivas B,Himanshu S.Determination of center-of-mass of gravity recovery and climate experiment satellites[J].Journal of Spacecraft and Rockets,2010,47(2):371-379
[22]廖鹤,赵艳彬,孙克新,等.质量特性调整机构在航天器中的应用[J].航天器环境工程,2009,26(2):168-171
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