DocumentCode :
2268311
Title :
Flexible coherent digital transceiver for low power space missions
Author :
Haskins, Christopher B. ; Millard, Wesley P. ; Jensen, J. Robert
Author_Institution :
Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD
fYear :
0
fDate :
0-0 0
Abstract :
A flexible coherent digital transceiver architecture has been developed by the APL in order to enable mission specific performance tailoring while maintaining modularity and minimizing program-incurred cost and risk. The new transceiver architecture is based on the heritage X-band transceiver system that is currently integrated into the New Horizons spacecraft. Using this new architecture, a low power, coherent, X-band digital transceiver has been made that meets the requirements for two-way Doppler tracking. The new transceiver contributes less than 0.01 mm/s to the Doppler velocity error measured over a 60-second interval in coherent mode. Secondary power consumption is 2.8 W in the uplink-only mode of operation including the reference oscillator. Transceiver designs on the TIMED, CONTOUR, and New Horizons spacecraft were noncoherent, which required downlink telemetry in order to support two-way Doppler tracking (Jensen, 1999). The addition of a coherent capability allows this new architecture to be used on missions where carrier-only Doppler tracking is desired. This paper provides a description of the new transceiver architecture and its demonstrated performance
Keywords :
low-power electronics; space communication links; space research; transceivers; 2.8 W; Doppler velocity error; New Horizons spacecraft; X-band transceiver system; flexible coherent digital transceiver; low power space missions; two-way Doppler tracking; Costs; Downlink; Radio navigation; Receivers; Satellite navigation systems; Space missions; Space vehicles; Telemetry; Transceivers; Transponders;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2006 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-9545-X
Type :
conf
DOI :
10.1109/AERO.2006.1655851
Filename :
1655851
Link To Document :
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