RELATIVE-MOTION APPROACH FOR DIFFERENTIAL CORRECTION IN ORBIT DETERMINATION

被引:0
|
作者
Sinclair, Andrew J. [1 ]
Lovell, T. Alan [1 ]
Horneman, Kenneth [2 ]
Harris, Andrew [3 ]
Sizemore, Alex [4 ]
机构
[1] Air Force Res Lab, Space Vehicles Directorate, 3550 Aberdeen Ave SE, Kirtland AFB, NM 87117 USA
[2] CNR, 3550 Aberdeen Ave SE, Kirtland AFB, NM 87117 USA
[3] Univ Colorado, Dept Aerosp Engn Sci, 429 UCB, Boulder, CO 80309 USA
[4] Univ Kansas, Dept Aerosp Engn, 1530 W 15th St, Lawrence, KS 66045 USA
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中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper describes an approach for differential correction for angles-only orbit determination based on relative motion. Relative-orbit determination has traditionally been formulated for a space-based sensor in close proximity to the observed object. However, these approaches can be generalized for a distant sensor, and the motion of the observed object is described relative to some proximate reference orbit. The relative-orbit solution is used to define a new reference orbit in the next iteration, reducing approximation error in the relative-motion dynamics. The presented approach utilizes available analytic relative-motion solutions and does not introduce any linearizing approximation in the measurements.
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页码:2065 / 2076
页数:12
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