中国空间科学技术

中国空间科学技术

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星上运动部件对气象卫星姿态影响的研究

刘蕊;王平;吕振铎;   

  1. 北京控制工程研究所,北京控制工程研究所,北京控制工程研究所 北京100080,北京100080,北京100080
  • 发布日期:2005-12-25

Effects of Spacecraft Movable Accessory on the Attitude of Meteorological Satellite

Liu Rui Wang Ping Lü Zhenduo(Beijing Institute of Control Engineering,Beijing 100080)   

  • Online:2005-12-25
  • Supported by:
    国家自然科学基金项目:90205008

被引次数

11

摘要： 以中国下一代静止轨道气象卫星为对象,分析了有效载荷扫描镜运动和太阳翼步进运动对卫星姿态的影响。结果表明,有效载荷的正常扫描运动和太阳翼的步进运动对卫星姿态的影响很小,但有效载荷的黑体校准运动对卫星姿态的影响很大,必须进行补偿控制,否则卫星有效载荷扫描镜的指向精度无法满足设计要求。

关键词: 太阳翼, 有效载荷, 卫星姿态控制, 地球静止轨道, 气象卫星

Abstract: With the background of the next generation of geostationary orbit meteorological satellite,the effect of payload mirror motion and solar array stepping motion are studied.The(simulation) results show that the effects of payload mirror regular scanning motion and the solar(array) stepping motion on the satellite attitude are very small.But the satellite attitude is deeply(affected) by payload backbody calibration,so the compensation must be required,otherwise the pointing performance of payload mirrors can not meet the demands of satellite.