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卫星热设计中β角在不同轨道下的变化规律分析
引用本文:赵欣.卫星热设计中β角在不同轨道下的变化规律分析[J].航天器工程,2008,17(3):57-61.
作者姓名:赵欣
作者单位:北京空间飞行器总体设计部,北京,100094
摘    要:阳光矢量与卫星轨道平面之间夹角是卫星热控设计中至关重要的一个设计参数,其不仅与到达卫星表面的阳光热流密度密切相关,也与到达卫星表面的地球反射热流密度密切相关。文章根据β角的变化规律将传统意义上的轨道分为了同步轨道和非同步轨道两种,并结合升黄赤经夹角的变化规律分析了不同轨道下β角的变化规律,以及相应的热设计特点。

关 键 词:热控设计  β角  升黄赤经夹角  轨道倾角
文章编号:1673-8748(2008)03-0057-05
修稿时间:2007年10月31

Study on Change Rule of β Angle for Various Orbits in Satellite Thermal Design
ZHAO Xin.Study on Change Rule of β Angle for Various Orbits in Satellite Thermal Design[J].Spacecraft Engineering,2008,17(3):57-61.
Authors:ZHAO Xin
Institution:ZHAO Xin (Beijing Institute of Spacecraft System Engineering ,Beijing 100094,China)
Abstract:β angle is an important parameter in the satellite thermal design. It plays an important role in not only calculation of total incident solar flux directly from the Sun but also that of solar flux reflected from the Earth surface. Considering the change rule of β angle, a variety of orbits can be generally categorized as synchronous orbit and non-synchronous orbit. According to the change rule of the angle between right ascension of the ascending node(RAAN)and right ascen sion of the Sun(RAS),this paper further discusses the change rule of β angle in various types of orbits and analyzes the feature of thermal design in corresponding orbits.
Keywords:thermal design  β angle  the angle between RAAN and RAS  orbit inclination
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