Deep impact navigation system performance

被引:32
作者
Frauenholz, Raymond B. [1 ]
Bhat, Ramachandra S. [1 ]
Chesley, Steven R. [1 ]
Mastrodemos, Nickolaos [1 ]
Owen, William M., Jr. [1 ]
Ryne, Mark S. [1 ]
机构
[1] CALTECH, Jet Prop Lab, Deep Impact Navitat Team Chief, Pasadena, CA 91109 USA
关键词
D O I
10.2514/1.24310
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Deep Impact successfully met its primary mission objective on 4 July 2005 when the smart impactor guided itself into the path of Comet 9P/Tempel 1. The mother flyby spacecraft then observed and recorded the breathtaking collision and subsequent plume development. Ground-based navigators. targeted the prerelease trajectory using optical navigation image planning and data analysis, trajectory correction maneuver design and evaluation, and orbit determination using both radiometric and optical data. In-flight improvements to the Tempel 1 ephemeris were also a critical part of the overall navigation design and operations success. The achieved navigation accuracy established a new standard for comet encounters, and this difficult task taught several important lessons. This definitive work provides a mission overview, summarizes the navigation requirements, compares the achieved navigation performance with a baseline design that reflects in-flight updates, and identifies operational procedures that may benefit future confet-bound navigators.
引用
收藏
页码:39 / 56
页数:18
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