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| Symbol |
Meaning
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| acf |
autocorrelation function
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| AMC |
Advanced Media Calibration system (see Section 4.3)
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| DOY |
day-of-year, i.e. January 20 = DOY 020
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| DSN |
Deep Space Network, the NASA/JPL spacecraft communications and
tracking network with antennas at complexes in Australia, Spain, and
the United States
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| DSS |
Deep Space Station (identifier for specific antennas in the DSN, e.g.,
“DSS 25”)
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| f |
Fourier frequency
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| FTS |
Frequency and Timing System, the reference for two-way Doppler
tracking
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| Ka-band |
a deep space communications frequency 32 GHz
(for Cassini, “Ka1” is the downlink referenced to the X-band uplink;
“Ka2” is the downlink referenced to the Ka-band uplink)
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| KaT |
Cassini’s “Ka-band Translator” which accepts an uplink Ka-band
signal and phase-coherently translates it to a downlink Ka-band signal
for retransmission to earth
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| LISA |
Laser Interferometer Space Antenna, a future low-frequency GW
observatory [24 ]
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| one-way |
Doppler tracking where the downlink is referenced to an oscillator on
the spacecraft
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| pdf |
probability density function [83 ]
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| S-band |
a deep space communications frequency 2.3 GHz
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| scintillation |
phase fluctuation due to wave propagation in a random medium [100 ,
75 , 37 , 92 , 65 ]
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| SEP angle |
sun-earth-probe angle, the apparent solar elongation angle of the
spacecraft
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| Sx(f) |
power spectrum of x(t), i.e. Fourier transform of [67 ,
84 ]
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| T |
duration of an observation
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| T2 |
two-way light time between earth and spacecraft
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| three-way |
Doppler tracking where the received downlink is coherently referenced
to an uplink signal from another station
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| two-way |
Doppler tracking where the downlink is coherently referenced to the
uplink signal
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| X-band |
a deep space communications frequency 8.4 GHz
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x y |
convolution of time series x(t) and y(t) [32]
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| y(t) |
generic time series of fractional frequency, [23 ]
( : time series of two-way Doppler fractional frequency)
( : time series of three-way Doppler fractional frequency)
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radio frequency
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Allan deviation, fractional frequency stability at integration time
[23 ]
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angle between GW propagation direction and earth-spacecraft vector;
= cos( )
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