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MMS 3 Electron Drift Instrument (EDI) Ambient Electron Flux, Projection Method 1 (PM2), Level 2 (L2), Survey Mode, 31.25 ms Data

(2022). MMS 3 Electron Drift Instrument (EDI) Ambient Electron Flux, Projection Method 1 (PM2), Level 2 (L2), Survey Mode, 31.25 ms Data [Data set]. NASA Space Physics Data Facility. https://doi.org/10.48322/k30r-dp97 (CiteAs link). Accessed on .

ResourceID
spase://NASA/NumericalData/MMS/3/FIELDS/EDI/Survey/Level2/ElectronFluxAmbient/ProjectionMethod2/PT0.03125S

Description

Electron Drift Instrument (EDI) Ambient Survey, Level 2, 0.03125 s Data (32 samples/s). EDI has two scientific data acquisition modes, called electric field mode and ambient mode. In electric field mode, two coded electron beams are emitted such that they return to the detectors after one or more gyrations in the ambient magnetic and electric field. The firing directions and times-of-flight allow the derivation of the drift velocity and electric field. In ambient mode, the electron beams are not used. The detectors with their large geometric factors and their ability to adjust the field of view quickly allow continuous sampling of ambient electrons at a selected pitch angle and fixed but selectable energy. To find the beam directions that will hit the detector, EDI sweeps each beam in the plane perpendicular to B at a fixed angular rate of 0.22 °/ms until a signal has been acquired by the detector. Once signal has been acquired, the beams are swept back and forth to stay on target. Beam detection is not determined from the changes in the count-rates directly, but from the square of the beam counts divided by the background counts from ambient electrons, i.e., from the square of the instantaneous signal-to-noise ratio (SNR). This quantity is computed from data provided by the correlator in the Gun-Detector Electronics that also generates the coding pattern imposed on the outgoing beams. If the squared SNR ratio exceeds a threshold, this is taken as evidence that the beam is returning to the detector. The thresholds for SNR are chosen dependent on background fluxes. They represent a compromise between getting false hits (induced by strong variations in background electron fluxes) and missing true beam hits. The basic software loop that controls EDI operations is executed every 2 ms. As the times when the beams hit their detectors are neither synchronized with the telemetry nor equidistant, EDI data have no fixed time-resolution. Data are reported in telemetry slots. In Survey, using the standard packing mode 0, there are eight telemetry slots per second and Gyn Detector Unit (GDU). The last beam detected during the previous slot will be reported in the current slot. If no beam has been detected, the data quality will be set to zero. In Burst telemetry there are 128 slots per second and GDU. The data in each slot consists of information regarding the beam firing directions (stored in the form of analytic gun deflection voltages), times-of-flight (if successfully measured), quality indicators, time stamps of the beam hits, and some auxiliary correlator-related information. Whenever EDI is not in electron drift mode, it uses its ambient electron mode. The mode has the capability to sample at either 90 degrees pitch angle or at 0/180 degrees (field aligned), or to alternate between 90 degrees and field aligned with selectable dwell times. While all options have been demonstrated during the commissioning phase, only the field aligned mode has been used in the routine operations phase. The choices for energy are 250 eV, 500 eV, and 1 keV. The two detectors, which are facing opposite hemispheres, are looking strictly into opposite directions, so while one detector is looking along B the other is looking antiparallel to B (corresponding to pitch angles of 180 and 0 degrees, respectively). The two detectors switch roles every half spin of the spacecraft as the tip of the magnetic field vector spins outside the field of view of one detector and into the field of view of the other detector. Starting January 4, 2016, the anodes were chosen such that the projection of the magnetic field vector was best aligned with the center of the first (that is, outer) of the four anodes. This provides coverage of a larger range of pitch angles in general. Data taken in this configuration are identified by the term "amb-pm2" in the data product names. In the burst data where four channels (corresponding to the four adjacent sensor anode pads) are sampled per GDU, channel 1 represents best the pitch angle of 0 degrees (or 180 degrees). The EDI instrument paper can be found at: http://link.springer.com/article/10.1007%2Fs11214-015-0182-7. The EDI instrument data products guide can be found at https://lasp.colorado.edu/mms/sdc/public/datasets/fields/.

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Details

Version:2.5.0

NumericalData

ResourceID
spase://NASA/NumericalData/MMS/3/FIELDS/EDI/Survey/Level2/ElectronFluxAmbient/ProjectionMethod2/PT0.03125S
ResourceHeader
ResourceName
MMS 3 Electron Drift Instrument (EDI) Ambient Electron Flux, Projection Method 1 (PM2), Level 2 (L2), Survey Mode, 31.25 ms Data
AlternateName
MMS3_EDI_SRVY_L2_AMB-PM2
DOI
https://doi.org/10.48322/k30r-dp97
ReleaseDate
2023-03-04 12:34:56.789
RevisionHistory
RevisionEvent
ReleaseDate
2021-04-27 15:38:11
Note
Only known prior ReleaseDate of the metadata
RevisionEvent
ReleaseDate
2022-08-04 12:34:56.789
Note
Added DOI and PublicationInfo minted by LFB, updated the RepositoryID, updated the SPDF MetadataContact Person to Robert M. Candey, metadata updated to SPASE 2.4.1, reviewed by LFB 20220803
RevisionEvent
ReleaseDate
2023-03-04 12:34:56.789
Note
Standardized the ResourceName Format, Set AlternateName equal to the ProductKey, Revised the Acknowledgement, PublicationInfo Authors, and Contact Person list per request of the MMS EDI team, metadata updated to SPASE 2.5.0, reviewed by LFB 20230304
Description

Electron Drift Instrument (EDI) Ambient Survey, Level 2, 0.03125 s Data (32 samples/s). EDI has two scientific data acquisition modes, called electric field mode and ambient mode. In electric field mode, two coded electron beams are emitted such that they return to the detectors after one or more gyrations in the ambient magnetic and electric field. The firing directions and times-of-flight allow the derivation of the drift velocity and electric field. In ambient mode, the electron beams are not used. The detectors with their large geometric factors and their ability to adjust the field of view quickly allow continuous sampling of ambient electrons at a selected pitch angle and fixed but selectable energy. To find the beam directions that will hit the detector, EDI sweeps each beam in the plane perpendicular to B at a fixed angular rate of 0.22 °/ms until a signal has been acquired by the detector. Once signal has been acquired, the beams are swept back and forth to stay on target. Beam detection is not determined from the changes in the count-rates directly, but from the square of the beam counts divided by the background counts from ambient electrons, i.e., from the square of the instantaneous signal-to-noise ratio (SNR). This quantity is computed from data provided by the correlator in the Gun-Detector Electronics that also generates the coding pattern imposed on the outgoing beams. If the squared SNR ratio exceeds a threshold, this is taken as evidence that the beam is returning to the detector. The thresholds for SNR are chosen dependent on background fluxes. They represent a compromise between getting false hits (induced by strong variations in background electron fluxes) and missing true beam hits. The basic software loop that controls EDI operations is executed every 2 ms. As the times when the beams hit their detectors are neither synchronized with the telemetry nor equidistant, EDI data have no fixed time-resolution. Data are reported in telemetry slots. In Survey, using the standard packing mode 0, there are eight telemetry slots per second and Gyn Detector Unit (GDU). The last beam detected during the previous slot will be reported in the current slot. If no beam has been detected, the data quality will be set to zero. In Burst telemetry there are 128 slots per second and GDU. The data in each slot consists of information regarding the beam firing directions (stored in the form of analytic gun deflection voltages), times-of-flight (if successfully measured), quality indicators, time stamps of the beam hits, and some auxiliary correlator-related information. Whenever EDI is not in electron drift mode, it uses its ambient electron mode. The mode has the capability to sample at either 90 degrees pitch angle or at 0/180 degrees (field aligned), or to alternate between 90 degrees and field aligned with selectable dwell times. While all options have been demonstrated during the commissioning phase, only the field aligned mode has been used in the routine operations phase. The choices for energy are 250 eV, 500 eV, and 1 keV. The two detectors, which are facing opposite hemispheres, are looking strictly into opposite directions, so while one detector is looking along B the other is looking antiparallel to B (corresponding to pitch angles of 180 and 0 degrees, respectively). The two detectors switch roles every half spin of the spacecraft as the tip of the magnetic field vector spins outside the field of view of one detector and into the field of view of the other detector. Starting January 4, 2016, the anodes were chosen such that the projection of the magnetic field vector was best aligned with the center of the first (that is, outer) of the four anodes. This provides coverage of a larger range of pitch angles in general. Data taken in this configuration are identified by the term "amb-pm2" in the data product names. In the burst data where four channels (corresponding to the four adjacent sensor anode pads) are sampled per GDU, channel 1 represents best the pitch angle of 0 degrees (or 180 degrees). The EDI instrument paper can be found at: http://link.springer.com/article/10.1007%2Fs11214-015-0182-7. The EDI instrument data products guide can be found at https://lasp.colorado.edu/mms/sdc/public/datasets/fields/.

Acknowledgement
Please acknowledge R.B. Torbert, M.R. Argall, and J.L. Burch for use of these data
PublicationInfo
Authors
Torbert, Roy, B.; Argall, Matthew, R.; Burch, James, L.
PublicationDate
2022-01-01 00:00:00
PublishedBy
NASA Space Physics Data Facility
Contacts
RolePersonStartDateStopDateNote
1.InstrumentLead
CoInvestigator
spase://SMWG/Person/Roy.B.Torbert
2.Developerspase://SMWG/Person/Matthew.R.ArgallGroundSoftwareDeveloper
3.PrincipalInvestigatorspase://SMWG/Person/James.L.Burch
4.HostContactspase://SMWG/Person/MMS_SDC_POC
5.MetadataContactspase://SMWG/Person/Robert.M.Candey
6.MetadataContactspase://SMWG/Person/Lee.Frost.Bargatze
InformationURL
Name
The Magnetospheric Multiscale (MMS) Mission home page at Goddard Space Flight Center (GSFC)
URL
Description

The Magnetospheric Multiscale (MMS) Mission Home Page hosted by the Goddard Space Flight Center (GSFC).

InformationURL
Name
Data Caveats and Current Release Notes at LASP MMS SDC
URL
Description

The Magnetospheric Multiscale (MMS) Mission home page hosted by the Laboratory of Atmospheric and Space Physics, Science Data Center (LASP, SDC) at the University of Colorado, Boulder.

InformationURL
Name
At UNH
URL
Description

The Magnetospheric Multiscale (MMS) FIELDS Instrument Suite home page. The web page is hosted by the University of New Hampshire (UNH).

PriorIDs
spase://VSPO/NumericalData/MMS/3/FIELDS/EDI/Survey/Level2/ElectronFluxAmbient/ProjectionMethod2/PT0.03125S
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
FTPS from the MMS SDC (not with most browsers)
URL
Description

In CDF via ftp from the MMS Science Data Center

AccessURL
Name
HTTPS from the MMS SDC
URL
Description

In CDF via http from the MMS Science Data Center

Format
CDF
Encoding
None
Acknowledgement
Please acknowledge R.B. Torbert, M.R. Argall, and J.L. Burch. Also please acknowledge the data providers and CDAWeb when using these data.
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
FTPS from SPDF (not with most browsers)
URL
Description

In CDF via ftp from SPDF

AccessURL
Name
HTTPS from SPDF
URL
Description

In CDF via http from SPDF

AccessURL
Name
CDAWeb
URL
ProductKey
MMS3_EDI_SRVY_L2_AMB-PM2
Description

Access to ASCII, CDF, and plots via NASA/GSFC CDAWeb

Format
CDF
Encoding
None
Acknowledgement
Please acknowledge R.B. Torbert, M.R. Argall, and J.L. Burch. Also please acknowledge the data providers and CDAWeb when using these data.
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
CDAWeb HAPI Server
URL
Style
HAPI
ProductKey
MMS3_EDI_SRVY_L2_AMB-PM2
Description

Web Service to this product using the HAPI interface

Format
CSV
Acknowledgement
Please acknowledge R.B. Torbert, M.R. Argall, and J.L. Burch. Also please acknowledge the data providers and CDAWeb when using these data.
ProcessingLevel
Calibrated
InstrumentIDs
MeasurementType
EnergeticParticles
TemporalDescription
TimeSpan
StartDate
2016-01-05 00:00:00.000
RelativeStopDate
-P2M
Cadence
PT0.03125S
ObservedRegion
Earth.Magnetosheath
ObservedRegion
Earth.Magnetosphere
ObservedRegion
Earth.Magnetosphere.Magnetotail
ObservedRegion
Earth.Magnetosphere.Main
ObservedRegion
Earth.Magnetosphere.RadiationBelt
ObservedRegion
Earth.NearSurface.EquatorialRegion
ObservedRegion
Earth.NearSurface.Plasmasphere
ObservedRegion
Heliosphere.NearEarth
Parameter #1
Name
Epoch Time
ParameterKey
Epoch
Description

Epoch Time Tags for Electron Flux and Trajectories Data, Terrestrial Time 2000 (TT2000)

Cadence
PT0.03125S
Units
ns
UnitsConversion
1e-9>s
RenderingHints
AxisLabel
UT
ValueFormat
I16
ValidMin
2015-03-01T00:00:00.000000000
ValidMax
2065-12-31T00:00:01.000000000
FillValue
9999-12-31T23:59:59.999999999
Support
SupportQuantity
Temporal
Parameter #2
Name
Epoch Time Tag
ParameterKey
epoch_timetag
Description

Epoch Time Tags for EDU Support Data, Terrestrial Time 2000 (TT2000)

Cadence
PT0.03125S
Units
ns
UnitsConversion
1e-9>s
RenderingHints
AxisLabel
UT
ValueFormat
I16
ValidMin
2015-03-01T00:00:00.000000000
ValidMax
2065-12-31T00:00:01.000000000
FillValue
9999-12-31T23:59:59.999999999
Support
SupportQuantity
Temporal
Parameter #3
Name
Optics State
Set
Time series defined by using: EPOCH_TIMETAG
ParameterKey
mms3_edi_optics_state_srvy_l2
Description

Optics State Parameter Setting

Cadence
PT0.03125S
RenderingHints
AxisLabel
Optics
ValueFormat
I4
ValidMin
0
ValidMax
254
FillValue
255
Support
SupportQuantity
InstrumentMode
Parameter #4
Name
GDU1 Beam Energy
Set
Time series defined by using: EPOCH_TIMETAG
ParameterKey
mms3_edi_energy_gdu1_srvy_l2
Description

Gun Detector Unit 2 Beam Energy

Cadence
PT0.03125S
Units
eV
UnitsConversion
1.602e-19>J
RenderingHints
AxisLabel
Energy
ValueFormat
I4
ValidMin
0
ValidMax
1000
FillValue
65535
Particle
ParticleType
Electron
Qualifier
Scalar
ParticleQuantity
Energy
Parameter #5
Name
GDU2 Beam Energy
Set
Time series defined by using: EPOCH_TIMETAG
ParameterKey
mms3_edi_energy_gdu2_srvy_l2
Description

Gun Detector Unit 1 Beam Energy

Cadence
PT0.03125S
Units
eV
UnitsConversion
1.602e-19>J
RenderingHints
AxisLabel
Energy
ValueFormat
I4
ValidMin
0
ValidMax
1000
FillValue
65535
Particle
ParticleType
Electron
Qualifier
Scalar
ParticleQuantity
Energy
Parameter #6
Name
GDU Identifier, 0 degree, Pitch Angle
Set
Time series defined by using: EPOCH
ParameterKey
mms3_edi_gdu_0_srvy_l2
Description

Sorts 0 degree Flux Counts by Gun Detector Unit

Cadence
PT0.03125S
RenderingHints
ValueFormat
I1
ValidMin
1
ValidMax
2
FillValue
255
Particle
ParticleType
Electron
Qualifier
Scalar
ParticleQuantity
Counts
Parameter #7
Name
GDU Identifier, 180 degree, Pitch Angle
Set
Time series defined by using: EPOCH
ParameterKey
mms3_edi_gdu_180_srvy_l2
Description

Sorts 180 degree Flux Counts by Gun Detector Unit

Cadence
PT0.03125S
RenderingHints
ValueFormat
I1
ValidMin
1
ValidMax
2
FillValue
255
Particle
ParticleType
Electron
Qualifier
Scalar
ParticleQuantity
Counts
Parameter #8
Name
Electron Flux, Trajectory 1, 0 degree Pitch Angle
Set
Time series defined by using: EPOCH
ParameterKey
mms3_edi_flux1_0_srvy_l2
Description

Flux for Electrons with Trajectories given by traj1_0

Cadence
PT0.03125S
Units
cm^-2 s^-1
UnitsConversion
1e4>m^-2 s^-1
RenderingHints
DisplayType
TimeSeries
AxisLabel
Flux
ValueFormat
E12.5
ValidMin
0.0
ValidMax
1.0e+20
FillValue
-1.0e+31
Particle
ParticleType
Electron
Qualifier
Directional
ParticleQuantity
NumberFlux
Parameter #9
Name
Electron Flux, Trajectory 1, 180 degree Pitch Angle
Set
Time series defined by using: EPOCH
ParameterKey
mms3_edi_flux1_180_srvy_l2
Description

Flux for Electrons with Trajectories given by traj1_180

Cadence
PT0.03125S
Units
cm^-2 s^-1
UnitsConversion
1e4>m^-2 s^-1
RenderingHints
DisplayType
TimeSeries
AxisLabel
Flux
ValueFormat
E12.5
ValidMin
0.0
ValidMax
1.0e+20
FillValue
-1.0e+31
Particle
ParticleType
Electron
Qualifier
Directional
ParticleQuantity
NumberFlux
Parameter #10
Name
Electron Flux Error, Trajectory 1, 0 degree Pitch Angle
Set
Time series defined by using: EPOCH
ParameterKey
mms3_edi_flux1_0_delta_srvy_l2
Description

Error for flux1 0 degree Pitch Angle Electron Flux

Cadence
PT0.03125S
Units
cm^-2 s^-1
UnitsConversion
1e4>m^-2 s^-1
RenderingHints
AxisLabel
dFlux
ValueFormat
E12.5
ValidMin
0.0
ValidMax
1.0e+20
FillValue
-1.0e+31
Particle
ParticleType
Electron
Qualifier
Uncertainty
ParticleQuantity
NumberFlux
Parameter #11
Name
Electron Flux Error, Trajectory 1, 180 degree Pitch Angle
Set
Time series defined by using: EPOCH
ParameterKey
mms3_edi_flux1_180_delta_srvy_l2
Description

Error for flux1 180 degree Pitch Angle Electron Flux

Cadence
PT0.03125S
Units
cm^-2 s^-1
UnitsConversion
1e4>m^-2 s^-1
RenderingHints
AxisLabel
dFlux
ValueFormat
E12.5
ValidMin
0.0
ValidMax
1.0e+20
FillValue
-1.0e+31
Particle
ParticleType
Electron
Qualifier
Uncertainty
ParticleQuantity
NumberFlux
Parameter #12
Name
Electron Trajectory 1, 0 degree Pitch Angle (GSE)
Set
Time series defined by using: EPOCH
ParameterKey
mms3_edi_traj1_gse_0_srvy_l2
Description

Trajectory of flux1 0 degree Pitch Angle Electrons in Geocentric Solar Ecliptic (GSE) Cartesian Coordinates

Caveats
Trajectories are given as unit vectors in spherical coordinates, with phi (theta) representing the azimuthal (polar) directions, in the indicated coordinate system. They are opposite to the nominal look-direction of the instrument. Errors represent an omni-directional error. For more details about errors, contact the EDI instrument team.
Cadence
PT0.03125S
Units
degree
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
DisplayType
TimeSeries
ValueFormat
F9.4
ScaleType
LinearScale
Structure
Size
2
Element
Name
Phi
Index
1
Element
Name
Theta
Index
2
ValidMin
-180.0
ValidMax
180.0
FillValue
-1.0e+31
Particle
ParticleType
Electron
ParticleQuantity
ArrivalDirection
Parameter #13
Name
Electron Trajectory 1, 180 degree Pitch Angle (GSE)
Set
Time series defined by using: EPOCH
ParameterKey
mms3_edi_traj1_gse_180_srvy_l2
Description

Trajectory of flux1 180 degree Pitch Angle Electrons in Geocentric Solar Ecliptic (GSE) Cartesian Coordinates

Caveats
Trajectories are given as unit vectors in spherical coordinates, with phi (theta) representing the azimuthal (polar) directions, in the indicated coordinate system. They are opposite to the nominal look-direction of the instrument. Errors represent an omni-directional error. For more details about errors, contact the EDI instrument team.
Cadence
PT0.03125S
Units
degree
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSE
RenderingHints
DisplayType
TimeSeries
ValueFormat
F9.4
ScaleType
LinearScale
Structure
Size
2
Element
Name
Phi
Index
1
Element
Name
Theta
Index
2
ValidMin
-180.0
ValidMax
180.0
FillValue
-1.0e+31
Particle
ParticleType
Electron
ParticleQuantity
ArrivalDirection
Parameter #14
Name
Electron Trajectory 1, 0 degree Pitch Angle (GSM)
Set
Time series defined by using: EPOCH
ParameterKey
mms3_edi_traj1_gsm_0_srvy_l2
Description

Trajectory of flux1 0 degree Pitch Angle Electrons in Geocentric Solar Magnetospheric (GSM) Cartesian Coordinates

Caveats
Trajectories are given as unit vectors in spherical coordinates, with phi (theta) representing the azimuthal (polar) directions, in the indicated coordinate system. They are opposite to the nominal look-direction of the instrument. Errors represent an omni-directional error. For more details about errors, contact the EDI instrument team.
Cadence
PT0.03125S
Units
degree
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSM
RenderingHints
DisplayType
TimeSeries
ValueFormat
F9.4
ScaleType
LinearScale
Structure
Size
2
Element
Name
Phi
Index
1
Element
Name
Theta
Index
2
ValidMin
-180.0
ValidMax
180.0
FillValue
-1.0e+31
Particle
ParticleType
Electron
ParticleQuantity
ArrivalDirection
Parameter #15
Name
Electron Trajectory 1, 180 degree Pitch Angle (GSM)
Set
Time series defined by using: EPOCH
ParameterKey
mms3_edi_traj1_gsm_180_srvy_l2
Description

Trajectory of flux1 180 degree Pitch Angle Electrons in Geocentric Solar Magnetospheric (GSM) Cartesian Coordinates

Caveats
Trajectories are given as unit vectors in spherical coordinates, with phi (theta) representing the azimuthal (polar) directions, in the indicated coordinate system. They are opposite to the nominal look-direction of the instrument. Errors represent an omni-directional error. For more details about errors, contact the EDI instrument team.
Cadence
PT0.03125S
Units
degree
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GSM
RenderingHints
DisplayType
TimeSeries
ValueFormat
F9.4
ScaleType
LinearScale
Structure
Size
2
Element
Name
Phi
Index
1
Element
Name
Theta
Index
2
ValidMin
-20.0
ValidMax
20.0
FillValue
-1.0e+31
Particle
ParticleType
Electron
ParticleQuantity
ArrivalDirection