DocumentCode
2101899
Title
Model of receiver design flaw - crucial for Huygens space mission recovery
Author
Popken, L.
Author_Institution
ESA-ESTEC, Noordwijk, Netherlands
Volume
2
fYear
2004
fDate
6-13 March 2004
Firstpage
1408
Abstract
An analytical model is presented to recover from a current design flaw in the Huygens space mission relay-link receiver. The model of the faulty implementation of a data transition tracking loop (DTTL) is a driver for the trajectory redesign leading to the new relay-link geometry of the Huygens mission. This recovery shall allow for a successful data retrieval from the probe during its descent towards the Saturn Moon Titan, despite the tracking deficiency in the given symbol synchronizer. The model of the DTTL implementation is presented in terms of system-level parameters: link performance (Es/No), symbol transition density Pt, and input symbol-rate offset ΔF. The analytical model has undergone extensive successful verification during in-orbit tests and performance mappings since the discovery of the anomaly.
Keywords
Saturn; radio receivers; space communication links; synchronisation; Huygens space mission recovery; Huygens space mission relay-link receiver; Titan Saturn Moon; data retrieval; data transition tracking loop; in-orbit tests; receiver design flaw model; relay link geometry; symbol rate offset; symbol synchronizer; symbol transition density; system level parameters; Analytical models; Geometry; Information retrieval; Probes; Relays; Saturn; Solid modeling; Space missions; Tracking loops; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2004. Proceedings. 2004 IEEE
ISSN
1095-323X
Print_ISBN
0-7803-8155-6
Type
conf
DOI
10.1109/AERO.2004.1367742
Filename
1367742
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