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在轨地球同步卫星地球敏感器干扰及指向计算
引用本文:祝转民,李于衡.在轨地球同步卫星地球敏感器干扰及指向计算[J].上海航天,2007,24(4):38-42.
作者姓名:祝转民  李于衡
作者单位:1. 西安交通大学,理学院,陕西,西安,710049
2. 西安电子科技大学,综合业务网国家重点实验室,陕西,西安,710071
摘    要:从工程应用角度,基于太阳、月球位置和卫星轨道根数推导了太阳和月球对地球同步轨道卫星红外地球敏感器干扰的计算公式及预报方法,同时给出了安全模式下卫星Z轴跟踪太阳时星上天线指向变化的计算模型。计算结果和卫星下传遥测数据验证了方法的正确性,可用于实际卫星管理。

关 键 词:地球同步轨道卫星  地球敏感器  太阳干扰  月球干扰  天线指向
文章编号:1006-1630(2007)04-0038-05
收稿时间:2006-06-21
修稿时间:2006-07-28

Computing Earth-Sensor Interference and Antenna Pointing for On-Orbit Satellite
ZHU Zhuan-min,LI Yu-heng.Computing Earth-Sensor Interference and Antenna Pointing for On-Orbit Satellite[J].Aerospace Shanghai,2007,24(4):38-42.
Authors:ZHU Zhuan-min  LI Yu-heng
Abstract:The formulas to predict the interference of the sun and moon with the infrared earth sensor of geostationary orbit satellite and the prediction method were derived based on the positions of the sun and moon and orbit elements of the satellite in engineering in this paper.The computation model was presented of the angle change for the antenna when the Z axis of the on-orbit satellite tracing the sun to ensure the power supply in safety model.The calculation results and telemetry data downloaded from the satellite showed that this method was correct,which would be applied in satellite's operation management.
Keywords:Geostationary orbit satellite  Infrared earth sensor  Sun interference  Moon interference  Antenna pointing
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