A SOLUTION TO THE THREE-BODY LAMBERT PROBLEM BASED ON CUBATURE KALMAN FILTER PARAMETER ESTIMATION

被引：0

作者：

Zhao, Qichen ^{[1
]}

Zhang, Hongli ^{[2
]}

Zhang, Ran ^{[1
]}

Han, Chao ^{[1
]}

机构：

[1] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China

[2] Beijing Electromech Engn Inst, Beijing 100000, Peoples R China

来源：

SPACEFLIGHT MECHANICS 2017, PTS I - IV | 2017年 / 160卷

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The three-body Lambert problem is to find out an orbit determined from two position vectors and transfer time in the three-body system. Its solution is generally divided into two steps: initial guess based on the two-body model and final solution using cubature kalman filter parameter estimation (CPE). CPE is based on the theory of probability without the gradient matrixes which are hard to calculate. Moreover, by using CPE the demand for the accuracy of the initial values for the three-body Lambert problem is modified. Results show CPE is efficient, robust and has a larger convergence domain compared with other methods.

引用

页码：3939 / 3950

页数：12

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