DocumentCode
2788990
Title
An advanced synthesized ultra-stable oscillator for spacecraft applications
Author
Wallis, Robert E. ; Weaver, Gregory L. ; Reinhart, Matthew J. ; Cheng, Sheng
Author_Institution
Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
fYear
2005
fDate
5-12 March 2005
Firstpage
952
Lastpage
960
Abstract
Current ultra-stable oscillator (USO) technology relies on highly precise quartz resonators that are selected based on the desired output frequency and stability. These constraints on the crystal specifications significantly increase the lead time and expense of each USO. Recent research and development efforts in USOs by The Johns Hopkins University Applied Physics Laboratory (JHU/APL) have focused on a frequency synthesized USO based on a standardized, fixed-frequency resonator. The result of these efforts is a synthesized USO that will provide a frequency reference for transponders and other on-board users on future space missions. The frequency reference is stable enough for radio-science and navigation applications (Allan deviation <1.5 × 10-13 at τ = 10 s), and is electronically adjustable to cover the entire deep-space communications band. This frequency agility allows in flight re-assignment of the transponder frequencies. The synthesized USO offers low mass and DC power consumption yet maintains world-class noise performance and frequency stability performance.
Keywords
crystal resonators; oscillators; space vehicle electronics; transponders; advanced synthesized ultra-stable oscillator; crystal specifications; deep-space communications band; fixed-frequency resonator; frequency agility; frequency reference; quartz resonators; space missions; spacecraft applications; transponder frequencies; Frequency synthesizers; Laboratories; Oscillators; Physics; Research and development; Space missions; Space technology; Space vehicles; Stability; Transponders;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2005 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-8870-4
Type
conf
DOI
10.1109/AERO.2005.1559386
Filename
1559386
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