A Simple Lambert Algorithm

被引:76
作者
Avanzini, Giulio [1 ]
机构
[1] Politecn Torino, Dept Aerosp Engn, I-10129 Turin, Italy
关键词
D O I
10.2514/1.36426
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A classic result for the two-point boundary value problem in the framework of Keplerian motion allows the derivation of a novel parametrization of orbits passing through two arbitrary points in space. In particular, it is shown that these orbits can.be unambiguously identified in terms of their eccentricity vector component in the direction perpendicular to the chord connecting the two points. The parametrization, in terms of transverse eccentricity component, lends itself to an efficient and intuitive solution algorithm for the classical Lambert problem, that is, the determination of the orbit that connects two points in space in a prescribed time. Although, from the computational point of view, the resulting numerical procedure does not provide advantages over the elegant Battin's method, its derivation is considerably less demanding from the mathematical standpoint and physically more intuitive.
引用
收藏
页码:1587 / 1594
页数:8
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