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遥感卫星高精度高稳定度控制技术
引用本文:边志强,蔡陈生,吕旺,沈毅力.遥感卫星高精度高稳定度控制技术[J].上海航天,2014,31(3):24-33,38.
作者姓名:边志强  蔡陈生  吕旺  沈毅力
作者单位:[1]上海卫星工程研究所,上海200240 [2]上海航天控制技术研究所,上海200233
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。

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

High Accuracy and High Stability Control Technology of Remote Sensing Satellite
BIAN Zhi-qiang,CAI Chen-sheng,LV Wang,SHEN Yi-li.High Accuracy and High Stability Control Technology of Remote Sensing Satellite[J].Aerospace Shanghai,2014,31(3):24-33,38.
Authors:BIAN Zhi-qiang  CAI Chen-sheng  LV Wang  SHEN Yi-li
Institution:1. Shanghai Institute of Satellite Engineering, Shanghai 200240, China; 2. Shanghai Institute of Spaceflight Control Technology, Shanghai 200233, China)
Abstract: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.
Keywords:Remote sensing satellite  Flexible multi-body dynamics  High accuracy and high stability  Attitude control
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