Maneuver estimation model for relative orbit determination

被引：0
|
作者：
Storch, Tara R. [1 ]
Wiesel, William E. [1 ]
Sabol, Chris [1 ]
Alfriend, Kyle T. [1 ]
Luu, K. Kim [1 ]
机构：
[1] SWC, 730 Irwin Ave Ste 83, Schriever AFB, CO 80912 USA
来源：
ASTRODYNAMICS 2005, VOL 123, PTS 1-3 | 2006年 / 123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：
This research investigated relative orbit determination of individual satellites within a cluster, focusing on instances when a maneuver has been detected or suspected. Developed using non-linear least squares estimation, the maneuver model estimates magnitude, direction, and time of a suspected maneuver. Observations for the DirecTV 4S and AMC-4 satellite collocation were obtained from the Air Force Maui Optical and Supercomputing (AMOS) site consisting of differential right ascension and declination. Dynamics are modeled using Hill's equations.
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收藏
页码：2457 / +
页数：2
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