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Research ArticleOriginal Article
Open Access

Formulation and Characterization of One-Way Radiometric Tracking with the Iris Radio Using a Chip-Scale Atomic Clock

Todd Ely, Zaid Towfic, and Dana Sorensen
NAVIGATION: Journal of the Institute of Navigation March 2024, 71 (1) navi.633; DOI: https://doi.org/10.33012/navi.633
Todd Ely
1Jet Propulsion Laboratory, California Institute of Technology
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Zaid Towfic,
1Jet Propulsion Laboratory, California Institute of Technology
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Dana Sorensen
2Space Dynamics Laboratory
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  • FIGURE 1
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    FIGURE 1

    Block diagram of Iris radio signal processing for forming one-way uplink radiometric data

  • FIGURE 2
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    FIGURE 2

    Iris DDC

  • FIGURE 3
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    FIGURE 3

    1σ range error uncertainty from the Iris STL for various loop bandwidths as a function of range signal power to noise (Pr/No)

  • FIGURE 4
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    FIGURE 4

    Difference between Iris time and CSAC time (left) and the second difference (right)

  • FIGURE 5
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    FIGURE 5

    Raw total count phase

  • FIGURE 6
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    FIGURE 6

    OADs of the raw total count phase, the same phase with its frequency drift removed, and the calibrated phase for Method 1, all normalized by the carrier frequency

  • FIGURE 7
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    FIGURE 7

    One-way range rate uncertainty as determined using Method 1

    The theoretical result is computed using the RSS of Equations (41)–(43), and the experimental result is the standard deviation of the range rate residuals after the removal of deterministic biases, rates, and accelerations.

  • FIGURE 8
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    FIGURE 8

    OAD of the range rate computed using Method 1 for selected integration times

  • FIGURE 9
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    FIGURE 9

    Range rate results for Method 1 with T =1 s; range rate from the uncalibrated phase (top), calibrated range rate (middle), and calibrated range with bias, rate, and acceleration effects removed (i.e., “detrended”) (bottom)

  • FIGURE 10
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    FIGURE 10

    Histogram of the calibrated, detrended range rate for Method 1 with T =1 s

  • FIGURE 11
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    FIGURE 11

    Range rate results for Method 1 with T =60 s; range rate from the uncalibrated phase (top), calibrated range rate (middle), and calibrated range with bias, rate, and acceleration effects removed (i.e., “detrended”) (bottom)

  • FIGURE 12
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    FIGURE 12

    Histogram of the calibrated, detrended range rate for Method 1 with T =60 s

  • FIGURE 13
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    FIGURE 13

    Prefit clock residuals (top) and postfit residuals (bottom)

  • FIGURE 14
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    FIGURE 14

    OAD of the clock filter prefit residuals (blue), postfit residuals (orange), clock phase solution (green), and normalized raw total count phase (red)

  • FIGURE 15
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    FIGURE 15

    OADs of the raw total count phase (blue), the same phase with its frequency drift removed (orange), the calibrated phase based on Method 2 (green), and, for comparison, the calibrated phase based on Method 1 (red), all normalized by the identified carrier frequency

  • FIGURE 16
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    FIGURE 16

    One-way range rate uncertainty as determined via Method 2

    The theoretical result (orange dash–dot curve) is computed from Equation (60), and the experimental result (blue curve) is the standard deviation of the range rate residuals after the removal of deterministic biases, rates, and accelerations. Experimental results for Method 1 (green curve) are shown for comparison.

  • FIGURE 17
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    FIGURE 17

    OAD of the range rate computed from Method 2 for selected integration times

  • FIGURE 18
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    FIGURE 18

    Range rate results for Method 2 with T =1 and 60 s

    The top and bottom left images are for T =1 s, and the top and bottom right images are for T =60 s. Top plots show the range rate from the uncalibrated phase (top), calibrated range rate (middle), and calibrated range with bias, rate, and acceleration effects removed (i.e., “detrended”) (bottom) for their respective integration times. Bottom plots show an associated histogram of the calibrated and detrended range rates.

  • FIGURE 19
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    FIGURE 19

    Iris TCXO range results: raw (upper left) and detrended (lower left); CSAC range results: raw (upper right) and detrended (lower right)

  • FIGURE 20
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    FIGURE 20

    OAD of the raw CSAC range (blue) and raw Iris TCXO range (orange), which have both been normalized to time by dividing by the speed of light; CSAC (green) and TCXO (red) OAD derived from total count phase measurements

  • FIGURE 21
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    FIGURE 21

    Iris CTL

  • FIGURE 22
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    FIGURE 22

    Iris STL used for ranging demodulation in the discrete time domain (top) and a continuous linear representation in the s-domain where VCO is a voltage controlled oscillator (bottom)

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    TABLE 1

    Relevant Iris Telemetry Fields for Computing Time and Total Count Phase

    Field NameSizeDescription
    1PPS Count4 bytesRunning integral count of 1PPS seconds, which can accumulate up to 232 seconds (or approximately 136 years)
    Iris Time (seconds)4 bytesCount of seconds since Iris was turned on based on TCXO ticks; increments each time the subseconds counter rolls over
    Iris Time (subseconds)4 bytesCount of 50-MHz TCXO ticks; rolls over to 0 after 49,999,999
    Total Carrier Phase (TCP)8 bytesIntegral number representing the total count phase since carrier lock; determines a floating-point estimate of phase cycles using Embedded Image
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    TABLE 2

    Iris TCXO and CSAC Allan Deviation, Aging, and Noise Specifications

    Allan Deviation σy(T)aσWFσRWF
    Iris TCXO (Q-Tech Q804)Spec value:
    • σy(1) < 1 × 10−19

    8.1 ×10−9/day – 2.4 ×10−8/dayEmbedded ImageEmbedded Image
    Measured values:
    • σy(1) = 4 × 10−11

    • σy(100) = 5 × 10−11

    • σy(1000) = 2 × 10−10

    • σy(10000) = 2 × 10−9

    (Variation as seen with measured OAD for different tests)(Derived from measured OAD)(Derived from measured OAD)
    CSAC SA-45SSpec values:
    • σy(1) = 3 × 10−10

    • σy(10) = 1 × 10−10

    • σy (100) = 3 × 10−11

    • σy(1000) = 1 × 10−11

    Embedded Image
    (Derived from specified OAD)
    Embedded Image
    (Derived from specified OAD)
    Embedded Image
    (Derived from specified OAD)
    Measured values:
    • Unknown

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    TABLE 3

    Relevant Iris Telemetry Fields for Computing PN Range

    Field NameSizeDescription
    PN Epoch Count4 bytesIndex of PN epoch; increments each time PN chip 0 is received; count begins when the PN ranging correlators are locked; resets to 0 when lock is lost; rolls over to 0 after 65,535
    PN Chip Index (q)4 bytesPN component sequence delays; can be used to calculate index of current PN chip (0 to 1,009,469) using the Chinese remainder theorem; valid when PN ranging correlators are locked
    PN Chip Accumulator (PCA)8 bytesPN symbol clock phase accumulator from the STL; accumulation begins when the PN ranging correlators are locked; determines a floating-point estimate of the fractional chip phase using Embedded Image
    ETT Epoch4 bytesPN epoch count to which the current value of the ETT register belongs
    ETT4 bytes32-bit ETT; bit 31 corresponds to the bit encoded in PN chip 0 of the epoch reported in the ETT epoch register
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    TABLE 4

    Estimated Fractional Frequency Offsets and Aging for the Iris TCXO and CSAC Determined From Range

    Embedded ImageEmbedded Image
    Iris TCXO6.07 × 10−7 s/s, 1821 m/s8.1 × 10−9/day, 2.8 × 10−5 m/s2
    CSAC1.50 × 10−9 s/s, 0.45 m/s5.8 × 10−11/day, 2.0 × 10−7 m/s2

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NAVIGATION: Journal of the Institute of Navigation: 71 (1)
NAVIGATION: Journal of the Institute of Navigation
Vol. 71, Issue 1
Spring 2024
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Formulation and Characterization of One-Way Radiometric Tracking with the Iris Radio Using a Chip-Scale Atomic Clock
Todd Ely, Zaid Towfic,, Dana Sorensen
NAVIGATION: Journal of the Institute of Navigation Mar 2024, 71 (1) navi.633; DOI: 10.33012/navi.633

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Formulation and Characterization of One-Way Radiometric Tracking with the Iris Radio Using a Chip-Scale Atomic Clock
Todd Ely, Zaid Towfic,, Dana Sorensen
NAVIGATION: Journal of the Institute of Navigation Mar 2024, 71 (1) navi.633; DOI: 10.33012/navi.633
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  • Article
    • Abstract
    • 1 INTRODUCTION
    • 2 IRIS RADIO RECEIVER SIGNAL PROCESSING TO OBTAIN THE TOTAL COUNT PHASE
    • 3 FORMING THE RANGE RATE MEASUREMENTS
    • 4 IRIS RADIO RECEIVER SIGNAL PROCESSING TO OBTAIN RANGE
    • 5 RANGE RATE RESULTS FROM THE TWO METHODS
    • 6 RANGE RESULTS
    • HOW TO CITE THIS ARTICLE
    • ACKNOWLEDGEMENTS
    • APPENDIX A: IRIS CARRIER PHASE NOISE VARIANCE
    • APPENDIX B: IRIS SYMBOL TIMING VARIANCE
    • Footnotes
    • REFERENCES
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Keywords

  • autonomous navigation
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  • iris radio
  • radiometric tracking

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