期刊文献+

高分四号卫星控制方案设计特点及在轨实现 被引量:5

Highlights of Attitude and Orbit Control System(AOCS) for Gao Fen-4 Satellite with On-Orbit Verification
下载PDF
导出
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. GF4 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 GaoFen4 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.
出处 《空间控制技术与应用》 CSCD 北大核心 2016年第6期1-8,共8页 Aerospace Control and Application
基金 国家自然科学基金资助项目(61473037)
关键词 地球静止轨道 光学遥感 高分辨率 姿轨控制 GEO remote sensing high resolution attitude and orbit control
  • 相关文献

参考文献2

二级参考文献15

  • 1Kozai Y. A J, 1959, 64(9): 367
  • 2Cook G E. Celest Mech, 1973, 7(3): 301
  • 3ENNIS G, JIM B, JOE D, et al. Overview of the optical design and performance of the high resolution science imaging experiment (HiRISE) [J]. SHE, 2005, 5874: 1-10.
  • 4GREGORY T H, ABEL J, MANDI J. Thermal design considerations of the Hubble Space Telescope (HST) science instrument control and data handler (SIC&DH 2)[C]//Proceedings of the 40th ICES, Pittsburgh: SAE, 2010: 1-8.
  • 5YU ZHEN, ZHONG CHENXING, GUO YU. Spectral analysis and parameter selection for BCB attitude maneuver path of flexible spacecraft [C]. International Conference on Information and Automation (ICIA), Yinchuan, August 26-28, 2013: 729-734.
  • 6GUO YANNING, SONG BIN, MA GUANGFU. Attitude maneuver control of two-flywheel spacecraft using potential function method [C]. Control Conference (CCC) Chinese, Xiran, July 26-28, 2013: 5132-5137.
  • 7GUI HAICHAO, JIN LEI. Attitude maneuver control of a two-wheeled spacecraft with hounded wheel speeds [J]. Acta Astronautica, 2013, 88: 98-107.
  • 8SHANG MENGYAO, ZHANG TAO, SONG JINGYAN. Optimal torque control constraint rigid spacecraft attitude maneuver with constraints [C]. Control Conference (CCC) Chinese, Xian, July 26-28, 2013: 363-367.
  • 9徐开,金光,陈娟,陈长青.敏捷小卫星姿态机动切换算法[J].光学精密工程,2008,16(8):1528-1532. 被引量:15
  • 10贾学志,金光,张雷.空间相机外遮光罩结构设计与优化[J].光学精密工程,2008,16(8):1560-1565. 被引量:24

共引文献20

同被引文献29

引证文献5

二级引证文献8

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部