三次样条在卫星轨道插值中的应用研究Research of boundary conditions of cubic spline interpolation applications in satellite orbit and velocity
黄旭方,韦义宏,唐秋玲,陈俊江
摘要(Abstract):
针对在卫星轨道插值中三次样条插值法的端点约束条件不易获得的问题,提出两种获得端点一阶导数的计算方法:差分法代替导数法;利用位置、速度和加速度之间的导数关系,求解坐标和速度的一阶导数。通过算例仿真表明,两种方法的坐标插值误差达毫米级以上,速度插值误差达厘米级以上,它们的插值精度均不受分段弧长影响,且比7阶Lagrange插值精度要高,但它们的运算时间比7阶拉格朗日插值法略大。其中,方法一优于方法二,因前者的速度插值误差比后者小,且后者的插值结果存在周期性抖动现象,其抖动周期与抽样频率有关。文中方法具有插值精度高,插值精度不受分段弧长影响,运算量不大的优点,是一种实用的卫星轨道和速度插值方法。
关键词(KeyWords): 插值;边界条件;卫星轨道;卫星速度
基金项目(Foundation): 国家自然科学基金项目(61563004);; 南宁市科技攻关项目(20141033);; 广西教育厅重点项目(ZD2014003)
作者(Author): 黄旭方,韦义宏,唐秋玲,陈俊江
DOI: 10.16251/j.cnki.1009-2307.2017.01.018
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