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.

引用

页码：2457 / +

页数：2

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