The method of least squares used to invert an orbit problem
The method of least squares used to invert an orbit problem
复制标题
用于反演轨道问题的最小二乘法
DOI:
10.1119/1.1613270
复制
发表时间:
2003
影响因子:
0.9
通讯作者:
R. Bannister
中科院分区:
文献类型:
--
作者:
R. Bannister
Six parameters uniquely describe the orbit of a body about the Sun. Given these parameters, it is possible to make predictions of the body’s position by solving its equation of motion. The parameters cannot be directly measured, so they must be inferred indirectly by an inversion method which uses measurements of other quantities in combination with the equation of motion. Inverse techniques are valuable tools in many applications where only noisy, incomplete, and indirect observations are available for estimating parameter values. The methodology of the approach is introduced and the Kepler problem is used as a real-world example.