DocumentCode :
2287709
Title :
Operations comparison of deep space ranging types: Sequential tone vs. pseudo-noise
Author :
Berner, J.B. ; Bryant, Scott H.
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume :
3
fYear :
2002
fDate :
2002
Abstract :
NASA´s Deep Space Network currently has a ranging system that uses a sequence of square wave tones to determine spacecraft distance. This ranging system correlates tones received from the spacecraft with those it transmitted. The phase shift that maximizes the correlation value is then related to the round trip light time distance. A new ranging system is being developed that can be configured to use sequential square wave tones or to use repeating pseudonoise tones. This allows more flexibility and possibly better performance. The tradeoffs between the two types of ranging are presented. A detailed derivation of the ranging performance as a function of configuration, signal strength, and other variables is given. The ranging performance for the two ranging types is compared. A configuration for pseudo-noise ranging that provides better performance is provided. Operational issues and simplifications resulting from using pseudo-noise ranging are also discussed.
Keywords :
correlation methods; distance measurement; pseudonoise codes; radionavigation; sequential codes; space communication links; NASA Deep Space Network; flexibility; operations comparison; phase shift; pseudo-noise deep space ranging; pseudo-noise ranging; ranging configuration; ranging performance; ranging system; received/transmitted tone correlation; repeating pseudo-noise tones; round trip light time distance; sequential square wave tones; sequential tone deep space ranging; signal strength; spacecraft distance; square wave tone sequence; Downlink; Earth; Frequency; Laboratories; Postal services; Propulsion; Receiving antennas; Space vehicles; Transmitting antennas; Transponders;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
Type :
conf
DOI :
10.1109/AERO.2002.1035264
Filename :
1035264
Link To Document :
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