【摘要】 研究了斜飞斜装太阳同步轨道卫星太阳帆板驱动律。通过坐标系变换,根据确定的太阳帆板开始驱动时刻及地球阴影区,基于MATLAB\Simulink\RTW软件的仿真数值设计法,设计了某斜飞斜装太阳同步轨道卫星的太阳帆板驱动律。结果表明:所设计的卫太阳帆板驱动律可满足工程需要。该法具一定的参考价值。更多还原

【Abstract】 The driving laws of sun synchronous orbit(SSO) satellite that aviated slantingly with a pair of slanting solar arrays were studied in this paper.According to the driving starting time of solar arrays and the(earth’s) shadow area, the driving laws of some SSO satellite with slanting solar array were designed through coordinate system transform based on a numerical design method using MATLAB\Simulink\RTW software.The results showed that the designed driving laws of the solar arrays would meet the requirement of engineering.The method was valuable.更多还原