OPTICAL NAVIGATION CONCEPT OF OPERATIONS FOR THE OSIRIS-REX MISSION

被引：0

作者：

Jackman, Coralie D. ^{[1
]}

Nelson, Derek S. ^{[1
]}

McCarthy, Leilah K. ^{[1
]}

Finley, Tiffany J. ^{[2
]}

Liounis, Andrew J. ^{[3
]}

Getzandanner, Kenneth M. ^{[2
]}

Antreasian, Peter G. ^{[1
]}

Moreau, Michael C. ^{[2
]}

机构：

[1] KinetX Inc, Space Nav & Flight Dynam Practice, 21 W Easy St,Ste 108, Simi Valley, CA 93065 USA

[2] Southwest Res Inst, 1050 Walnut St,Suite 300, Boulder, CO 80302 USA

[3] NASA, Goddard Space Flight Ctr, Nav & Mission Design Branch, Code 595, Greenbelt, MD 20771 USA

来源：

SPACEFLIGHT MECHANICS 2017, PTS I - IV | 2017年 / 160卷

基金：

美国国家航空航天局;

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：

The OSIRIS-REx sample return mission will begin proximity operations at asteroid Bennu in late 2018. Optical Navigation (OpNav), a sub-function of the Flight Dynamics System, uses information extracted from spacecraft images to assist in the orbit determination of the spacecraft. Star-based OpNav is utilized in early mission phases, before global imaging data and digital terrain maps are available. Once these maps are available, landmark navigation is utilized in order to achieve the required navigation performance requirements. This paper will discuss the optical navigation concept of operations for each mission phase, details about imaging plans, and operational OpNav techniques.

引用

页码：3337 / 3354

页数：18

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