RELATIVE NAVIGATION FOR SATELLITES IN CLOSE PROXIMITY USING ANGLES-ONLY OBSERVATIONS

被引：0

作者：

Patel, Hemanshu ^{[1
]}

Lovell, T. Alan ^{[2
]}

Allgeier, Shawn ^{[3
]}

Russell, Ryan ^{[4
]}

Sinclair, Andrew ^{[5
]}

机构：

[1] Emergent Space Technol, Greenbelt, MD 20770 USA

[2] Air Force Res Lab, Kirtland AFB, NM USA

[3] Schafer Corp, Albuquerque, NM USA

[4] Univ Texas Austin, Dept Aerosp Engn & Engn Mech, Austin, TX 78712 USA

[5] Auburn Univ, Dept Aerosp Engn, Auburn, AL 36849 USA

来源：

SPACEFLIGHT MECHANICS 2012 | 2012年 / 143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：

Relative navigation using angles-only observations is explored in this research. Previous work has shown that the unique relative orbit of a deputy satellite cannot be found using angles-only camera measurements from the chief satellite when a linear model of relative motion is used, due to a lack of observability. This work examines the possibility of partial observability, which in this case consists of a basis vector that corresponds to a family of relative orbits. An initial orbit determination (IOD) method is introduced that uses 3 Line-Of-Sight (LOS) measurements and provides an initial guess for the basis vector. This guess is differentially corrected with a batch estimator that takes in a full set of LOS measurements to hone in on a converged solution for the basis vector.

引用

页码：1485 / +

页数：2

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