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The Parameterization of Top-Hat Particle Sensors with Microchannel-Plate-Based Detection Systems and its Application to the Fast Plasma Investigation on NASA's Magnetospheric MultiScale MissionThe most common instrument for low energy plasmas consists of a top-hat electrostatic analyzer geometry coupled with a microchannel-plate (MCP)-based detection system. While the electrostatic optics for such sensors are readily simulated and parameterized during the laboratory calibration process, the detection system is often less well characterized. Furthermore, due to finite resources, for large sensor suites such as the Fast Plasma Investigation (FPI) on NASA's Magnetospheric Multiscale (MMS) mission, calibration data are increasingly sparse. Measurements must be interpolated and extrapolated to understand instrument behavior for untestable operating modes and yet sensor inter-calibration is critical to mission success. To characterize instruments from a minimal set of parameters we have developed the first comprehensive mathematical description of both sensor electrostatic optics and particle detection systems. We include effects of MCP efficiency, gain, scattering, capacitive crosstalk, and charge cloud spreading at the detector output. Our parameterization enables the interpolation and extrapolation of instrument response to all relevant particle energies, detector high voltage settings, and polar angles from a small set of calibration data. We apply this model to the 32 sensor heads in the Dual Electron Sensor (DES) and 32 sensor heads in the Dual Ion Sensor (DIS) instruments on the 4 MMS observatories and use least squares fitting of calibration data to extract all key instrument parameters. Parameters that will evolve in flight, namely MCP gain, will be determined daily through application of this model to specifically tailored in-flight calibration activities, providing a robust characterization of sensor suite performance throughout mission lifetime. Beyond FPI, our model provides a valuable framework for the simulation and evaluation of future detection system designs and can be used to maximize instrument understanding with minimal calibration resources.
Document ID
20150011078
Acquisition Source
Goddard Space Flight Center
Document Type
Abstract
Authors
Gershman, Daniel J.
(Oak Ridge Associated Universities, Inc. Washington, DC, United States)
Gliese, Ulrik
(SGT, Inc. Greenbelt, MD, United States)
Dorelli, John C.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Avanov, Levon A.
(Maryland Univ. College Park, MD, United States)
Barrie, Alexander C.
(Millennium Engineering and Integration Co. Arlington, VA, United States)
Chornay, Dennis J.
(Maryland Univ. College Park, MD, United States)
MacDonald, Elizabeth A.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Holland, Matthew P.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Pollock, Craig J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
June 18, 2015
Publication Date
April 20, 2015
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
GSFC-E-DAA-TN21251
Report Number: GSFC-E-DAA-TN21251
Meeting Information
Meeting: Measurement Techniques in Solar and Space
Location: Boulder, CO
Country: United States
Start Date: April 20, 2015
End Date: April 24, 2015
Sponsors: NASA Headquarters, National Science Foundation
Funding Number(s)
CONTRACT_GRANT: NNG06EO90A
CONTRACT_GRANT: NNG12CR29C
CONTRACT_GRANT: NNH06CC03B
CONTRACT_GRANT: NNG12CR31C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Instrument-model
plasma-sensor
micro-channel-plate
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