A Keplerian approach to angles-only orbit determination

被引：0
|
作者：
Vitarius, Patrick J. [1 ]
Hahs, Daniel [1 ]
Gregory, Don A. [2 ]
机构：
[1] Freel Innovat Inc, 700 Blvd S SW,Suite 404, Huntsville, AL 35802 USA
[2] Univ Alabama, Dept Phys, Huntsville, AL 35899 USA
来源：
SPACEBORNE SENSORS III | 2006年 / 6220卷
关键词：
orbit determination; angles-only; 3D state vector estimation; orbital mechanics;
D O I：
10.1117/12.683828
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A method is derived from Kepler's laws of motion allowing the determination of slant range for orbiting targets given monocular angles-only measurements. The method is shown to work without knowledge of three parameters: universal gravitational constant, mass of the central body, and time scale. Monte Carlo trials with noisy data sets, however, show that the method is much more sensitive to measurement noise than competing methods that require knowledge of these parameters.
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收藏
页数：7
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