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2 Notation, Acronyms, and Conventions

Table 1UpdateJump To The Next Update Information defines some acronyms used in this article. Since it is always clear from context, I use the same symbol for theoretical statistical quantities (e.g., underlying spectra) and estimates derived from finite data sets (e.g., sample spectra). All power spectra are two-sided.


Table 1: Some acronyms and notation used in this paper.




Symbol

Meaning



   
acf

autocorrelation function

AMC

Advanced Media Calibration system (see Section 4.3)

DOY

day-of-year, i.e. January 20 = DOY 020

DSN

Deep Space Network, the NASA/JPL spacecraft communications and tracking network with antennas at complexes in Australia, Spain, and the United States

DSS

Deep Space Station (identifier for specific antennas in the DSN, e.g., “DSS 25”)

f

Fourier frequency

FTS

Frequency and Timing System, the reference for two-way Doppler tracking

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)

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

LISA

Laser Interferometer Space Antenna, a future low-frequency GW observatory [24Jump To The Next Citation Point]

one-way

Doppler tracking where the downlink is referenced to an oscillator on the spacecraft

pdf

probability density function [83Jump To The Next Citation Point]

S-band

a deep space communications frequency ≃ 2.3 GHz

scintillation

phase fluctuation due to wave propagation in a random medium [100Jump To The Next Citation Point,  75Jump To The Next Citation Point37Jump To The Next Citation Point92Jump To The Next Citation Point65Jump To The Next Citation Point]

SEP angle

sun-earth-probe angle, the apparent solar elongation angle of the spacecraft

Sx(f)

power spectrum of x(t), i.e. Fourier transform of ⟨x(t)x (t + τ)⟩ [67Jump To The Next Citation Point,  84Jump To The Next Citation Point]

T

duration of an observation

T2

two-way light time between earth and spacecraft

three-way

Doppler tracking where the received downlink is coherently referenced to an uplink signal from another station

two-way

Doppler tracking where the downlink is coherently referenced to the uplink signal

X-band

a deep space communications frequency ≃ 8.4 GHz

x ∗ y

convolution of time series x(t) and y(t) [32]

y(t)

generic time series of fractional frequency, Δ ν∕ν0 [23Jump To The Next Citation Point]
(y2(t): time series of two-way Doppler fractional frequency)
(y3(t): time series of three-way Doppler fractional frequency)

ν

radio frequency

σy (τ)

Allan deviation, fractional frequency stability at integration time τ [23Jump To The Next Citation Point]

θ

angle between GW propagation direction and earth-spacecraft vector; μ = cos(θ)





   


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