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
Link To Document :
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