高分四号卫星控制方案设计特点及在轨实现

doi:10.3969/j.issn.1674-1579.2016.06.001

摘要/Abstract

摘要： 高分四号(GF4)是首颗地球静止轨道光学面阵遥感卫星.简要综述了国外该领域发展情况，重点介绍了高分四号卫星控制系统方案设计的主要特点，包括全星敏转移轨道技术、姿态小角度步进机动与快速稳定、以及阳光规避技术，并结合实际飞行情况介绍了上述技术的在轨验证情况，最后对后续该领域技术发展提出了展望.

关键词: 地球静止轨道, 光学遥感, 高分辨率, 姿轨控制

Abstract: GF4 is the debut of high resolution remote sensing satellite on GEO. The technic development in this domain is briefed, and the highlights of AOCS for GaoFen4 satellite are detailed, including transfer orbit control via star tracker, attitude control with small angle step maneuvering and stabilizing, and sunlight avoiding control. Besides, the verifications of these technologies are also presented based on orbit flying data. The future technical developing trends are proposed finally.

Key words: GEO, remote sensing, high resolution； attitude and orbit control

中图分类号:

V448

. 高分四号卫星控制方案设计特点及在轨实现[J]. 空间控制技术与应用, 2016, 42(6): 1-7.

参考文献

［1］HOWARD E. NOAA’s future GOES satellite program［C］//GOES8 and Beyond Proceeding SPIE. Washington. D.C.: SPIE, 1996. ［2］HAILE W. GOESR preliminary jitter analysis［J］. Swales Aerospace. 2002, 3: 2029. ［3］MAX E N, JON F L. MONOLITHIC V. Deployable primary mirror trade considerations for the next generation space telescope［C］//Advanced Telescope Design, Fabrication and Control. SPIE, 2002. ［4］DANIEL R C, DAVID N J. Technology for the next generation space telescope［J］. SPIE, 2000(4013): 784794 ［5］BILIMORIA K D, WEI B. Timeoptimal threeaxis reorientation of a rigid spacecraft［J］. Journal of Guidance, Control, and Dynamics, 1993, 16: 446452. ［6］SCRIVENER S， THOMPSON R. Survey of time optimal attitude maneuvers［J］. Journal of Guidance， Control， and Dynamics， 1994, 17(2): 225233. ［7］BYERS R M, VADALI S R, JUNKINS J L, Nearminimum time, closedloopslewing of flexible spacecraft［J］. Journal of Guidance,Control,and Dynamics, 1990, 13(1): 5765. ［8］LI Y. Modeling and control of a flexible spacecraft for largeangle rapid maneuvers［J］. Automatic control in Aerospace, 1998： 341346. ［9］刘林, 王彦荣. 卫星轨道预报的一种分析方法［J］. 天文学报, 2005， 46(3): 307313. LIU L, WANG Y R. An analytical method for satellite orbit forecasting［J］. Acta Astronomica Sinica., 2005， 46(3): 307313. ［10］彭洲, 李振松, 乔国栋, 等. 地球静止轨道遥感卫星相机太阳规避设计［J］. 中国空间科学技术, 2015, 35(2): 5762. PENG Z, LI Z S, QIAO G D, et al. Sunlight avoidance design for camera of geostationary orbit remote sensing satellite［J］. Chinese Space Science and Technology, 2015, 35(2): 5762.

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