期刊文献+

遥感卫星高精度高稳定度控制技术 被引量:12

High Accuracy and High Stability Control Technology of Remote Sensing Satellite
下载PDF
导出
摘要 对遥感卫星高精度高稳定度控制技术进行了综述。给出了国内外高稳定度多挠性遥感卫星控制、快速机动控制、高精度姿态确定、自主智能控制等典型应用,以及未来发展趋势。分析了挠性多体卫星结构-控制一体化设计、卫星在轨试验和高精度姿态确定等关键技术。讨论了挠性多体卫星动力学建模仿真及地面试验验证,H∞控制、自适应滤波前馈等卫星姿态控制方法研究与应用,卫星结构模态与无干扰力矩在轨辨识,以及基于陀螺、星敏感器及其误差、卫星动力学模型、在轨热变形标定等高精度姿态确定技术。 The control technology with high accuracy and high stability of remote sensing satellite was summarized in this paper.The typical application of high stability control of multi-flexible satellite,fast maneuver control,high accuracy attitude determination and auto-intelligent control in the world,and the development trend in the future were given out.The key technologies that were the structure-control integrated design of multi-flexible satellite,on-orbit test and high accuracy attitude determination were analyzed.The dynamic modeling and simulation as well as ground test approval of multi-flexible satellite,the research and application of the satellite attitude control methods that were H∞ control,adoptive filtering front feedback,on-orbit identification of the satellite structure module and disturb torque,and the high accuracy attitude determination technology based on gyro,star sense and its error,dynamic model of satellite,on-orbit thermal deformation calibration were also discussed.
出处 《上海航天》 2014年第3期24-33,38,共11页 Aerospace Shanghai
关键词 遥感卫星 挠性多体动力学 高精度高稳定度 姿态控制 Remote sensing satellite Flexible multi-body dynamics High accuracy and high stability Attitude control
  • 相关文献

参考文献26

  • 1IRWIN R D,GLENN R D,FRAZIER W G,et al.Analytically and numerically derived H∞ controller design for Hubble space telescope[J].Journal of Guidance Control,and Dynamics,1995,18(2):214-221.
  • 2NURRE G S,SHARKEY J P,NELSON J J,et al.Preservicing mission,on-orbit modifications to Hub-ble space telescope pointing control system[J].Jour-nal of Guidance Control,and Dynamics,1995,18(2):222-229.
  • 3MOHL J B.Attitude determination and control for the Landsat spacecraft[R].AAS,92-011.
  • 4JEANNEAU M,ALAZARD D,MOUYON P.A semi-adaptive frequency control law for flexible struc-tures(on the way to adaptive Q LQG control)[R].AIAA,99-4229.
  • 5IWATA T.Attitude dynamics and disturbances of the advanced land observing satellite(ALOS):mod-eling,identification,and mitigation[R].AIAA,2008-6263.
  • 6IWATA T.Precision attitude and position determina-tion for the advanced land observing satellite(ALOS):SPIE 4th Int Asia-Pacific Environmental Remote Sensing Symp[C].Honolulu:2004.
  • 7李果.中国航天器未来发展的GNC关键技术[J].空间控制技术与应用,2009,35(6):1-5. 被引量:1
  • 8Doug Wiemer,何英姿.全球成像系统2000卫星的姿态确定与控制[J].控制工程(北京),2000(1):39-56. 被引量:1
  • 9曹海翊,刘希刚,李少辉,张新伟.“资源三号”卫星遥感技术[J].航天返回与遥感,2012,33(3):7-16. 被引量:43
  • 10许伟.快鸟-2卫星[J].国外卫星动态,2002(3):11-22. 被引量:1

二级参考文献68

共引文献101

同被引文献101

引证文献12

二级引证文献36

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