低轨低倾角卫星总体适应性方案研究  

Research on overall adaptability scheme of the low orbit and low inclination satellite

作　　者：叶小舟[1] 黄业平[1] 仲惟超[1] 沈庆丰[1] Ye Xiaozhou Huang Yeping Zhong Weichao Shen Qingfeng(Shanghai Institute of Satellite Engineering, Shanghai 201109, China)

机构地区：[1]上海卫星工程研究所,上海201109

出　　处：《航天电子对抗》2017年第3期16-18,58,共4页Aerospace Electronic Warfare

摘　　要：针对低轨低倾角卫星的复杂光照特性开展了深入分析,并论述了其对卫星总体设计的具体影响。基于轨道面光照角大动态周期变化规律,系统地提出了四种典型的卫星总体适应性方案并比对分析了各方案特点,最后结合载荷、任务等约束条件给出了方案选择建议。可作为低轨低倾角卫星的总体设计参考。The complex illumination characteristics of the low orbit and low inclination satellite are deeply analyzed. Based on the large dynamic periodic variation law of the orbital plane illumination angle, four typical satellite overall schemes are proposed systematically, and the characteristics of each scheme are compared and analyzed. Finally combined with the payloads, missions, etc. , the scheme selection proposal is given. It can be used as a design reference in the system design of the low orbit and low inclination satellite.

关 键 词：低轨 低倾角 卫星 偏航机动 对日定向 

分 类 号：V423.4[航空宇航科学与技术—飞行器设计]