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Characterizing an FPGA Based
Spectrometer Prototype for
Heterodyne Receivers at the LMT
By Tim costa
 Introduction
 Spectrometer Overview
 Characterization Tests
 OGP Calibration
 Linearity
 Allan Variance
 Future Work
 Summary
Overview
Background
SEQUOIA
The LMT
The Spectrometer
 FPGA based
 ROACH2
 Two ADC ports
 Each ADC has four cores with maximum sample rates
of 1.25 Gs/s1
The Spectrometer
 Offset/Gain/Phase (OGP) Calibration
 Linearity
 Allan Variance
Characterization Tests
 Aligning cores via OGP Calibration decreases the
effect of spurs
 Aligning cores increases signal to noise.
OGP Calibration
OGP Calibration
 Changes to input signal strength should result in a
corresponding change to output signal strength.
 Linearity is necessary for calibration.
Linearity
Linearity
Frequency
(MHz)
Noise Level (dB) Quantized Slope
100 -20 Yes 1.02 ± 0.03
200 -23 No 0.96 ± 0.01
400 -26 Yes 0.96 ± 0.07
799 -29 No 0.98 ±0.01
Linearity
 Spectrometers should follow the radiometer
equation
 σ α (b*t)-1/2
 Allan variance tests mimic weak signals in the
presence of high noise2
Allan Variance
Allan Variance
 Complete two more modes.
 400 Mhz
 200 Mhz
 Scale Up
 Integrate with OMAR
 Science at the LMT
Future Work
 OGP calibration eliminates spurs and improves S/N
 The spectrometer is linear until amplifiers in the ADCs
begin to saturate
 Allan time is at least 1000 seconds.
Summary
 Umass Amherst Department of Astronomy
 Five Colleges Astronomy Department
 Commonwealth Honors College
 Massachusetts Space Grant
I would especially like to thank Dr. Gopal Narayanan, my
thesis advisor, Aleks Popstefanija for his assistance with
Python, and Rurik Primiani of SAO for aspects of the
ASIAA ADC.
Acknowledgments
 https://upload.wikimedia.org/wikipedia/en/f/ff/FiveCollegeRadioObs.png
 http://www.astro.umass.edu/~fcrao/instrumentation/sequoia/seqhorns_
fixed_labeled.JPG
 http://astronomynow.com/wp-
content/uploads/2016/03/LMT_678x509.jpg
1.) e2v, “EV8AQ160 Quad ADC Datasheet DS0846”, 2016
2.) Schieder, R. & Kramer, C, “Optimization of Radio Astronomical
Observations Using Allan Variance Measurements”, 2001
3.) Patel, N. A. et al, “Characterizing the Performance of a High-Speed ADC
for the SMA Digital Backend”, 2014
References

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Thesis_powerpoint

Editor's Notes

  1. Five College Radio Astronomy Observatory (FCRAO) operated from 1969 until 2011 Hosted the Second Quabbin Observatory Imaging Array (SEQUOIA)
  2. Fastest imaging array at 3 mm wavelengths
  3. Largest active single dish telescope observing in the 0.85 to 4 mm wavelength range. Will have an active surface diameter of 50 m Currently lacks a focal plane array spectrometer
  4. Inclusion of the spectrometer will allow for the mapping of external galaxies and the mapping of several lines simultaneously. Multiple lines are needed for a full picture of the ISM and mapping multiple lines at the same time would save expensive telescope time allowing for more observations.
  5. FPGA designed by Collaboration for Astronomy Signal Processing and Electronics Research (CASPER) ROACH consists of a Xilinx Virtex-6 series FPGA, a PowerPC running Linux and two ADC docks Cores can be interleaved for a maximum sample rate of 5 Gs/s Largest bandwidth is 800 MHz, needs a Nyquist sampling frequency of at least 1600 MHz Our Spectrometer will have two pairs of two cores interleaved for a maximum sample rate of 2.5 Gs/s
  6. Aligning cores is all about time of samplers and amplifiers.
  7. Three graphs on the right have much more scatter than the three graphs on the left.
  8. And accurately measuring the system’s temperature
  9. Plotted are four different background noise levels, quantized and unquantized data, and several different frequencies. The turnoff occurs when the input signal hits a threshold, saturating amplifiers in the ADCs.
  10. This table contains a few parameters of some of the linearity test data. What’s important to note is that the slope of each of the lines is almost exactly one!
  11. Sigma is the noise, b is the bandwidth, and t is the integration time. When plotted in a log-log scale the noise should decrease linearly until Reality threshold is reached do to time variation in the gain causing the noise to increase after the Allan time.
  12. The Allan time is at least 1000 seconds
  13. Modes are bandwidths 15 more roaches for 16 pixels in total Omar (One Millimeter Array Receiver)