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弹道导弹扰动引力快速逼近的算法研究
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摘要
本研究系总参测绘局课题——远程导弹惯性制导系统的重力矢量实时测定系
    统——的一部分。全文围绕着远程导弹弹道点扰动引力的快速计算展开,主要讨
    论了四个方面的问题:首先是对现有扰动引力计算方法进行分析和比较,据此认
    为利用点质量模型和低价位系数模型组合法计算扰动引力是理论严密、计算精密
    的方法,并将它作为后面进一步研究的基础。其次,通过对常用数值逼近方法的
    考察,选取三次等距B样条函数对用上述方法计算出的某设计弹道的扰动引力进
    行了逼近,对结果进行分析后认为其适合于弹道扰动引力的快速计算。文章接着
    提出利用有限元内插方法对上述设计弹道的扰动引力进行逼近,重点集中在空间
    单元的剖分和单元形状函数的选取上,分析结果显示此方法也适合进行弹道扰动
    引力的快速计算。最后,对上面所得的算法进行了集成,编制了软件以满足实用
    中便捷和连续弹道计算的要求。
Revolving around the fast computation of the disturbing gravity of ballistic
    missile trajectory this dissertation mainly focuses on the following problems: firstly,
    analysis and comparison of the existing computing methods of the disturbing gravity
    are made, according to which the method of point mass model is considered strict and
    exact and thus is selected as the foundation of subsequent research; secondly, after a
    full review of the numerical interpolation methods in conunon use, because of its
    excellent property' the cubic isometrical B-spline is chosen to interpolate the
    disturbing gravity along some pre-designed trajectory and considered fit fOr the fast
    computation of disturbing gravity along a IIilssile trajectory after the analysis of
    result; thirdly, a finite element interpo1ation method is put forward in this paper, with
    emphasis laid on the partition of spatial elements and the selection of shaPe function
    of element, and consequent result shows that this method is also fit fOr the fast
    comPutation of disturbing gravity of IIilssile trajectory; finally, the above methods are
    integrated into software so as to be convenient and successive and automatic fOr
    further use.
引文
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