HPDE.io

Polar Electric Fields Instrument (EFI), Spacecraft Attitude in GSE coordinates

(2023). Polar Electric Fields Instrument (EFI), Spacecraft Attitude in GSE coordinates [Data set]. NASA Space Physics Data Facility. https://doi.org/10.48322/a4sb-1d04. Accessed on .

Note: Proper references, including those in BibTex or other formats, should include the "Accessed on date" as shown above to identify the version of the resource being cited in a given publication.

ResourceID
spase://NASA/NumericalData/POLAR/EFI/SC/GSE/Attitude/PT600S

Description

the Polar spacecraft positive spin axis direction vector (normalized to magnitude 1), in GSE coordinates.

View XML | View JSON | Edit

Details

Version:2.6.0

NumericalData

ResourceID
spase://NASA/NumericalData/POLAR/EFI/SC/GSE/Attitude/PT600S
ResourceHeader
ResourceName
Polar Electric Fields Instrument (EFI), Spacecraft Attitude in GSE coordinates
DOI
https://doi.org/10.48322/a4sb-1d04
ReleaseDate
2023-07-30 12:34:56.789
RevisionHistory
RevisionEvent
ReleaseDate
2021-04-27 15:38:11
Note
Only known prior ReleaseDate of the metadata
RevisionEvent
ReleaseDate
2023-07-30 12:34:56.789
Note
Added DOI and PublicationInfo minted by LFB, metadata versioned up to SPASE 2.6.0, reviewed by LFB 20230727
Description

the Polar spacecraft positive spin axis direction vector (normalized to magnitude 1), in GSE coordinates.

Acknowledgement
Please acknowledge the instrument PI, F.S. Mozer, and CDAWeb when using these data.
PublicationInfo
Authors
Mozer, Forrest, S.
PublicationDate
2023-01-01 00:00:00
PublishedBy
NASA Space Physics Data Facility
Contacts
RolePersonStartDateStopDateNote
1.PrincipalInvestigatorspase://SMWG/Person/Forrest.S.Mozer
2.MetadataContactspase://SMWG/Person/Jack.B.Vernetti
3.MetadataContactspase://SMWG/Person/Robert.E.McGuire
4.MetadataContactspase://SMWG/Person/Lee.Frost.Bargatze
PriorIDs
spase://VWO/NumericalData/POLAR/EFI/S_C_GSE_Attitude
spase://VSPO/NumericalData/POLAR/EFI/Attitude/PT10M
spase://VSPO/NumericalData/POLAR/EFI/SC/GSE/Attitude/PT600S
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
FTPS from SPDF (not with most browsers)
URL
Description

Access to Data in CDF Format via ftp from SPDF

AccessURL
Name
HTTPS from SPDF
URL
Description

Access to Data in CDF Format via http from SPDF

AccessURL
Name
CDAWeb
URL
ProductKey
PO_10MINATT_EFI
Description

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

Format
CDF
Encoding
None
Acknowledgement
Please acknowledge the instrument PI, F.S. Mozer, and CDAWeb when using these data.
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
CDAWeb HAPI Server
URL
Style
HAPI
ProductKey
PO_10MINATT_EFI
Description

Web Service to this product using the HAPI interface.

Format
CSV
Acknowledgement
Please acknowledge the instrument PI, F.S. Mozer, and CDAWeb when using these data.
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
POLAR EFI data archive
URL
Description

This URL is the root location of the POLAR EFI archive. It consists of Yearly subdirectories: 1996, 1997, ..., 2008 each of which consists of Monthly subdirectories: 01, 02, ..., 12 The archive files for a given date are located in the corresponding YY/MM subdirectory.

Language
en
Format
CDF
Encoding
None
Acknowledgement
The user will acknowledge, in any publication which uses POLAR EFI data, the instrument PI.
ProcessingLevel
Calibrated
InstrumentIDs
MeasurementType
Ephemeris
TemporalDescription
TimeSpan
StartDate
1996-03-16 00:00:00
StopDate
2008-04-13 24:00:00
Cadence
PT600S
ObservedRegion
Earth.Magnetosphere
ObservedRegion
Earth.Magnetosphere.Polar
ObservedRegion
Earth.NearSurface
ObservedRegion
Earth.NearSurface.AuroralRegion
ObservedRegion
Earth.NearSurface.EquatorialRegion
ObservedRegion
Earth.NearSurface.Ionosphere
ObservedRegion
Earth.NearSurface.PolarCap
Caveats
Important Warning: The Data described below is meant for Archival Purposes. It should not be considered as highly accurate Data. For example, Accurate Data requires a Correction in the Form of an Offset to the Sunward Component of the Electric Field. A Constant Offset of 1.2 mV/m has been used for all the Data this being an approximate Average Value. In fact, however, the Offset varies with Time and must be determined by Analysis of the particular Time of Interest. Users of these Data desiring more Information should get in touch with Dr. F.S. Mozer, at the Space Sciences Laboratory, University of California, Berkeley. The Electric Field Data is at Spin Period Time Resolution. This means that there is one Data Point about every 6 s. However, it should be noted that there can be longer Intervals between Data Points due to Missing Data. Data Gaps are not filled in. The Components of the Electric Field are given in a Coordinate System designated as Despun Spacecraft Coordinates, DSC. This is a Coordinate System for a rotating Spacecraft that is in an Orbit near the Earth. DSC is defined by the Spacecraft's Spin Plane and Spin Axis. However, as the Despun Part of the Name suggests, the Coordinate Axes do not participate in the Spacecraft's Rotation. The X-Axis and Y-Axis are on the Spacecraft's Spin Plane; the Z-Axis is along the Spacecraft's Spin Axis. The positive X, Y, and Z-Axes form an Orthogonal, Right-Handed Coordinate System. The positive Z-Axis points in the same Direction as the Spacecraft's Angular Momentum, or Spin or Attitude, Vector. The positive X-Axis points in the Direction in the Spin Plane that is closest to the Direction towards the Sun. In other Words, the positive X-Axis points in the Direction of the Projection on the Spin Plane of the Vector from the Spacecraft to the Sun. The positive Y-Axis is determined by the Requirement that the DSC XYZ System form an Orthogonal Right-Handed System. It follows that the positive Y-Axis points in the Direction on the Spin Plane that is 90 degrees ahead of the positive X-Axis in the Sense of the Spacecraft's Rotation. The Electric Field Data included in these Files consists of the two Electric Field Components in the Spin Plane. The Original Data used is V34L, which typically has a Time Resolution of about 40 Data Points per Second. A Least-Squares Spin Fit of V34L is performed and the Spin Fit Coefficients provide the Spin Plane Components of the Spin Period Electric Field. Time is a Real Double Precision Quantity. The Units for the Time are Seconds. The Time is the Time elapsed since the Epoch starting on May 24, 1968 at 00:00:00 UT. Each Time Tag indicates the Mid-Point of the Time Interval for the corresponding Spin Period. Data Gaps are not filled and each Time Tag corresponds to an Actual Data Point. X, Y, and Z are the three Components of the Attitude Vector in the Geocentric Solar Ecliptic, GSE, Coordinate System.
Parameter #1
Name
Time
ParameterKey
TIME_TAG
Description

Data point time-tags which are double precision floating point numbers which represent the number of seconds, UTC, from midnight of the day represented by the file.

Cadence
PT600S
Units
seconds
ValidMin
0.0
ValidMax
86460.0
Support
SupportQuantity
Temporal
Parameter #2
Name
SCAttitudeGSEVector
ParameterKey
DATA_VALUES
Description

Data point vector values which are a triplet of single precision floating point numbers which represent the normalized X,Y,Z components of the GSE spacecraft attitude (i.e. the direction of the spacecraft positive spin axis).

Cadence
PT600S
Units
Numeric
UnitsConversion
1.0
CoordinateSystem
CoordinateRepresentation
Cartesian
CoordinateSystemName
GSE
ValidMin
-1.0
ValidMax
1.0
Support
SupportQuantity
Positional