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倾斜轨道小卫星太阳高度角分析与机动方案设计
引用本文:丰保民,陈占胜,叶立军,季诚胜,朱虹. 倾斜轨道小卫星太阳高度角分析与机动方案设计[J]. 空间控制技术与应用, 2016, 42(3): 33-37
作者姓名:丰保民  陈占胜  叶立军  季诚胜  朱虹
作者单位:上海航天控制技术研究所,上海;上海市空间智能控制技术重点实验室,上海;上海航天技术研究院,上海;上海航天控制技术研究所,上海;上海市空间智能控制技术重点实验室,上海;上海航天控制技术研究所,上海;上海市空间智能控制技术重点实验室,上海;上海航天控制技术研究所,上海;上海市空间智能控制技术重点实验室,上海
基金项目:上海航天核攀资助项目(ZY2015 003 3)
摘    要:
针对倾斜轨道小卫星必然会面对的光学姿态敏感器受阳光干扰的问题,分析太阳高度角的变化规律,提出了计算太阳高度角的经验公式,并在此基础上提出了平台偏航姿态机动方案,可以使光学姿态敏感器规避阳光干扰,并可以简化整星热控和帆板驱动设计,提高了整星的可靠性.

关 键 词:倾斜轨道;太阳高度角;姿态机动

Solar Height Angle Analysis and Attitude ManeuverDesign of Inclined Orbit Small Satellite
FENG Baomin,CHEN Zhansheng,YE Lijun,JI Chengsheng and ZHU Hong. Solar Height Angle Analysis and Attitude ManeuverDesign of Inclined Orbit Small Satellite[J]. Aerospace Contrd and Application, 2016, 42(3): 33-37
Authors:FENG Baomin  CHEN Zhansheng  YE Lijun  JI Chengsheng  ZHU Hong
Affiliation:Shanghai Institute of Spaceflight Control Technology, Shanghai;Shanghai Key Laboratory of Aerospace Intelligent Control Technology, Shanghai;Shanghai Academy of Spaceflight Technology, Shanghai;Shanghai Institute of Spaceflight Control Technology, Shanghai;Shanghai Key Laboratory of Aerospace Intelligent Control Technology, Shanghai;Shanghai Institute of Spaceflight Control Technology, Shanghai;Shanghai Key Laboratory of Aerospace Intelligent Control Technology, Shanghai;Shanghai Institute of Spaceflight Control Technology, Shanghai;Shanghai Key Laboratory of Aerospace Intelligent Control Technology, Shanghai
Abstract:
Considering the optic attitude sensor of inclined orbit small satellite interfered by sunlight, the variation law of solar height angle is analyzed. For computing and analyzing easily, a handy experience formula of solar height angle is proposed. Based on the formula, a yaw axis attitude maneuver scheme is presented, which can avoid sunlight interferer and make thermal control design and solar array drive law design conveniently.
Keywords:inclined orbit   solar height angle   attitude maneuver
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