DocumentCode
990699
Title
Rescuing the Huygens Mission From Fiasco
Author
Popken, Luitjens
Author_Institution
Eur. Space Agency, Noordwijk
Volume
95
Issue
11
fYear
2007
Firstpage
2248
Lastpage
2258
Abstract
On January 14, 2005, the Huygens probe, which forms part of the joint NASA/ESA/ASI deep-space mission Cassini-Huygens, accomplished its spectacular descent through the atmosphere of Titan, Saturn´s largest moon. This mission success, however, became possible only after the rescue of the endeavor from an implementation flaw that was discovered in 2000 during an in-orbit test of the Huygens relay-link receiver. The problem threatened to cripple the entire $350 million probe mission. This paper presents the model of the faulty implementation of a data transition tracking loop. This model was the driver for the trajectory redesign leading to the revised relay-link geometry of the Huygens mission. The recovery eventually allowed for the data retrieval from the probe during its descent and after the landing on Titan, despite the tracking deficiency in the symbol synchronizer. The approach taken to identify and solve the communication problem is also an illustrative tutorial example of synchronization theory applied to save an entire space mission from disaster.
Keywords
radio receivers; space communication links; space vehicles; Huygens mission; data retrieval; data transition tracking loop; radio receiver flaw; relay-link geometry; space probe mission; symbol synchronizer; Atmosphere; Geometry; Moon; NASA; Probes; Relays; Saturn; Solid modeling; Testing; Tracking loops; Cassini orbiter; Huygens probe; Saturn; Titan; data transition tracking loop (DTTL); mission recovery; synchronization;
fLanguage
English
Journal_Title
Proceedings of the IEEE
Publisher
ieee
ISSN
0018-9219
Type
jour
DOI
10.1109/JPROC.2007.906629
Filename
4390044
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