User Interface Spec
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ResourceField NameData TypeWidget TypeDefault ValueRangeAccessDescriptionUnitsField CouplingsRequirements
Interfaces
Additional Tests
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AcceptFilterObservedObjectsObject ArrayN/A{All}User defined observed object or 'All'SetList of user-created tracked objects (e.g., name of the Spacecraft resource being tracked). This field can use to filter data in both TrackingFileSet and BatchEstimatorInv.N/ANoneFRR-48.2.1. It needs to add requirements for BatchEstimatorInv.S
3
AcceptFilterFileNamesString ArrayN/A{All}valid file name, 'All', or 'From_AddTrackingConfig'SetList of file names (a subset of the relevant TrackingFileSet's FileName field) containing the tracking data. This field can use to filter data in TrackingFileSet only.

If this field equals From_AddTrackingConfig, then two things happen; (1) All of the files in the relevant TrackFileSet are used as a starting point, and (2) Of the data in all of the files, only the data defined by the AddTrackingConfig field of the relevant TrackingFileSet are used.
N/ANoneFRR-48.2.7S
4
AcceptFilterTrackersObject ArrayN/A{All}any valid user-created Tracker object (e.g., GroundStation) or 'All'SetList of user-created trackers (e.g., name of the Ground Station being used). This field can use to filter data in both TrackingFileSet and BatchEstimatorInv.N/ANoneFRR-48.2.2 It needs to add requirements for BatchEstimatorInv.S
5
AcceptFilterDataTypesString ArrayN/A{All}Range, DSN_SeqRange, RangeRate, DSN_TCP, GPS_PosVec, or AllSetList of data types. This field can use to filter data in both TrackingFileSet and BatchEstimatorInv.N/ADataThinFRR-48.2.3. It needs to add requirements for BatchEstimatorInv.S
6
AcceptFilterEpochFormatStringN/ATAIModJulianUTCGregorian, UTCModJulian, TAIGregorian, TAIModJulian, TTGregorian, TTModJulian A1Gregorian, A1ModJulian, TDBGregorian, TDBModJulianSetAllows user to select format of the epoch. This field can use to filter data in both TrackingFileSet and BatchEstimatorInv.N/AInitialEpoch, FinalEpochFRR-48.2.4. It needs to add requirements for BatchEstimatorInv.S
7
AcceptFilterInitialEpochStringN/Aearliest day defined in GMATuser-defined initial epochSetInitial epoch of desired data. This field can use to filter data in both TrackingFileSet and BatchEstimatorInv.N/AEpochFormatFRR-48.2.4. It needs to add requirements for BatchEstimatorInv.S
8
AcceptFilterFinalEpochStringN/Alatest day defined in GMATuser-defined final epochSetFinal epoch of desired data. This field can use to filter data in both TrackingFileSet and BatchEstimatorInv.N/AEpochFormatFRR-48.2.4. It needs to add requirements for BatchEstimatorInv.S
9
AcceptFilterThinModeStringN/AFrequency"Frequency" or "Time"Set"Frequency" for record count frequency mode and "Time" for time window frequency mode. This field can use to fill data in TrackingFileSet only.N/AIt works associated with EpochFormat, InitialEpoch, and FinalEpochFRR-48.2.5, FRR-48.2.6S
10
AcceptFilterThinningFrequencyIntegerN/A1Positive integerSetIf ThinMode is Frequency, the integer 'n' is used to specify that every nth data point should be accepted. For example, 3 specifies that every third data point, meeting all the accept criteria, should be accepted and 1 specifies that every data point, meeting all the accept criteria, should be accepted. If ThinMode is Time, the integer 'n' is a number of seconds between accepted observations, using the first available observation as the anchor epoch. For example, a value of 300 means that observations will be accepted every 300 seconds, starting from the first available observation. This field can use to fill data in TrackingFileSet only.N/A or secondsIt works associated with EpochFormat, InitialEpoch, and FinalEpochFRR-48.2.5, FRR-48.2.6S
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AcceptFilterRecordNumbersString ArrayN/A{All}A list of all valid range of record numberSetThis field can use to filter data based on picked record numbers. This field can use to filter data in BatchEstimatorInv only.N/AIt needs to requirement here.S
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AntennaNo fields
13
BarycenterBodyNamesStringListSelection ListEarth, LunaCelestial Body. You cannot add bodies to the built-in SolarySystemBarycenter object.SetThe list of celestial bodies included in the barycenter. A Celestial Body can only appear once in the BodyNames list.N/ANoneFRR-18.1G+SNone
14
BarycenterOrbitColor
Integer Array or String
ColorPickerGoldAny color available from the Orbit Color Picker in GUI. Valid predefined color name or RGB triplet value between 0 and 255.SetAllows you to set available colors on user-defined Barycenter orbits. The barycenter orbits are
drawn using the OrbitView graphics resource. Colors on Barycenter object can be set
through a string or an integer array. For example: Setting a barycenter's orbit color to red can be done in the following
two ways: Barycenter.OrbitColor = Red or Barycenter.OrbitColor = [255 0 0]. This
field can be modified in the Mission Sequence as well.
N/AN/AFRR-18.3.0G+SNone
15
BarycenterTargetColor
Integer Array or String
ColorPickerDarkGrayAny color available from the Orbit Color Picker in GUI. Valid predefined color name or RGB triplet value between 0 and 255.SetAllows you to select available colors for Barycenter object's perturbing orbital trajectories that are
drawn during iterative processes such as Differential Correction
or Optimization. The target color can be identified through a
string or an integer array. For example: Setting a barycenter's
perturbing trajectory color to yellow can be done in
following two ways: Barycenter.TargetColor =
Yellow or Barycenter.TargetColor = [255 255
0] . This field can be modified in the Mission Sequence
as well.
N/AN/AFRR-18.3.1G+SNone
16
BatchEstimatorInv
AbsoluteTolRealN/A0.001Real > 0.SetAbsolute Weighted RMS convergence criteria toleranceNoneN/AFRR-22.1.5.2S
17
BatchEstimatorInv
RelativeTolRealN/A0.0001Real > 0.SetRelative Weighted RMS convergence criteria toleranceNoneN/AFRR-22.1.5.1S
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BatchEstimatorInv
PropagatorObjectN/ANULLvalid propagator objectSetSpecifies propagator object iused for batch estimationNoneN/AFRR-22.1.3S
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BatchEstimatorInv
MeasurementsObjectArrayN/Aempty listvalid TrackingFileSet objectSetSpecifies a list of measurements used for batch estimationNoneN/AFRR-22.1.4S
20
BatchEstimatorInv
ShowAllResidualsOn/OffN/AOnOn or OffSetAllows residuals plots to be shownNoneN/AFRR-22.1.9S
21
BatchEstimatorInv
ShowProgresstrue/falseN/Atruetrue or falseSetAllows detailed output of the batch estimator to be shown in the message windowNoneN/AFRR-22.2S
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BatchEstimatorInv
ReportStyleStringN/ANormalNormal, Concise, Verbose, DebugSetSpecifies the type of estimation report. The Normal style excludes reporting of observation TAI, partials, and frequency information.NoneN/AFRR-22.1.8.2S
23
BatchEstimatorInv
ReportFileStringN/A''BatchEstimatorInv' + instancename + '.data'string containing a valid file nameSetspecifies the name of estimation report fileNoneN/AFRR-22.1.8.1S
24
BatchEstimatorInv
MaximumIterationsIntegerN/A15any positive integerSetSpecifies maximum number of iterations allowed for batch estimationNoneN/AFRR-22.1.5.3S
25
BatchEstimatorInv
MaxConsecutiveDivergences
IntegerN/A3any positive integerSetSpecifies maximum number of consecutive diverging iterations allowed before batch estimation processing is stoppedNoneN/AFRR-22.1.5.4S
26
BatchEstimatorInv
OLSEMultiplicativeConstantRealN/A3.0Real > 0.0SetMultiplicative constant used for outer loop sigma editing (OLSE). NoneN/AFRR-22.1.2.1S
27
BatchEstimatorInv
OLSEAdditiveConstantRealN/A0.0any real numberSetAdditive constant used for outer loop sigma editing (OLSE). NoneN/AFRR-22.1.2.2S
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BatchEstimatorInv
OLSEInitialRMSSigmaRealN/A3000.0Real > 0.0SetInitial predicted root-mean-square value used for outer loop sigma editing (OLSE)NoneN/AFRR-22.1.2.3S
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BatchEstimatorInv
OLSEUseRMSPtrue/falseN/ATRUEtrue or falseSetSelect WRMS or WRMSP for OLSE sigma editingNoneN/AFRR-22.1.11
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BatchEstimatorInv
InverseAlgorithmStringN/AInternalInternal,Cholesky, SchurSetAlgorithm used to invert the normal equationsNoneN/AFRR-22.1.7S
31
BatchEstimatorInv
ResetBestRMSIfDivergingtrue/falseN/Afalse
true or falseSetIf set true and the estimation process has diverged, then the Best RMS is reset to the current RMS. NoneN/AFRR-22.1.5.5S
32
BatchEstimatorInv
UseInitialCovariance
true/falseN/Afalse
true or falseSetIf set true, a-priori error covariance term is added to the estimation cost function.NoneN/AFRR-22.1.1S
33
BatchEstimatorInv
EstimationEpochFormatStringN/A'FromParticipants''FromParticipants'SetSpecify time format used for EstimationEpoch. When it is set to 'FromParticipants', Time format is the format set to Spacecraft.EpochFormat NoneSpacecraft.EpochFormatFRR-22.1.6S
34
BatchEstimatorInv
EstimationEpochStringN/A'FromParticipants''FromParticipants'SetSpecify time at which estimation state is calculated. When it is set to 'FromParticipants', time for estimation is the value of Spacecraft.Epoch.NoneSpacecraft.EpochFRR-22.1.6S
35
BatchEstimatorInv
MatlabFileStringN/ANoneAny valid file nameSetFile name for the output MATLAB file. A value of None means that no MATLAB file will be output.N/AFRR-22.4
36
BatchEstimatorInv
DataFiltersStringArrayN/A{}
a list of user-defined AcceptFilter or RejectFilter resourceSetDefines filters to be applied to the data. One or more filters of either type may be specified. Every observation data filtered by a filter will not been used for estimation calculation but their data still shown up in estimation report file.N/ANoneFRR-22.1.10S
37
BatchEstimatorInv
FreezeMeasurementEditingBoolean_TypeN/Afalse
True or FalseSetFreeze batch estimator observation editing. If invoked, subsequent iterations will be prevented from editing additional data.N/ANoneFRR-22.1.12
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BatchEstimatorInv
FreezeIterationIntegerN/ASetSelected iteration at which to begin editing freeze. GMAT is prevented from performing additional observation editing on this and subsequent iterations.N/ANoneFRR-22.1.12
39
CelestialBodyFrameSpiceKernelNameStringArrayListLuna: {'..\data\planetary_coeff\moon_080317.tf'}Valid SPICE FK kernelSetList of SPICE FK files to load for this body. Used to define celestial body properties for use with ContactLocator and EclipseLocator.N/ANoneG+SNone
40
CelestialBodyEopFileNameFileNameN/A'Valid file typeSetFilename to specify EOP file for Earth. When not set, the file specified in the startup file is used. When set to empty string (the default), this field has no affect, and the file from the startup file is used. N/ANoneS
41
CelestialBodyPlanetarySpiceKernelNameStringArrayListEarth: {'..\data\planetary_coeff\earth_070425_370426_predict.bpc', '..\data\planetary_coeff\earth_720101_070426.bpc', '..\data\planetary_coeff\earth_000101_151228_151006.bpc'}
Luna: {'..\data\planetary_coeff\moon_pa_de421_1900-2050.bpc'}
Valid SPICE PCK kernelSetList of SPICE PCK files to load for this body. Used to define celestial body properties for use with ContactLocator and EclipseLocator.N/ANoneG+SNone
42
CelestialBodySpiceFrameIdStringText boxEarth: ITRF93
Luna: MOON_PA
Others: IAU_BODYNAME
StringSetSPICE id of body-fixed frame.N/ANoneG+SNone
43
CelestialBodyTextureMapFileName FileNameText box'../data/graphics/texture/GenericCelestialBody.jpg'Valid file of typeSetTexture map used in OrbitView graphics.N/ANoneFRR-16.2.4G+SNone
44
CelestialBodyEquatorialRadius RealText Box6378.1363Real > 0.SetThe body's equatorial radius.kmNoneFRR-16.2.2G+SNone
45
CelestialBodyFlattening RealText Box0.0033527Real >= 0SetThe body's polar flattening.N/ANoneFRR-16.2.3G+SNone
46
CelestialBodyMu RealText Box398600.4415Real > 0.SetThe body's gravitational parameter.km^3/s^2NoneFRR-16.2.1G+SNone
47
CelestialBodyNutationUpdateInterval RealText box60Real >=0SetThe interval between updates for Earth nutation matrix. If NutationUpdateInterval = 3600, then GMAT only updated nutation on an hourly basis.sec.NoneFRR-16.2.7G+S
48
CelestialBodyRotationConstant RealText box190.147RealSetThe body's spin angle at the orientation epoch.degOrientationEpoch FRR-16.7.5G+SNone
49
CelestialBodyRotationRate RealText box360.9856235RealSetThe body's spin rate.deg/dayNoneFRR-16.7.6G+SNone
50
CelestialBodySpinAxisDECConstant RealText box90RealSetThe declination of the body's spin axis at the orientation epoch.degOrientationEpoch FRR-16.7.3G+SNone
51
CelestialBodySpinAxisDECRate RealText box -0.5570RealSetThe rate of change of the body's declination.deg/centuryNoneFRR-16.7.1G+SNone
52
CelestialBodySpinAxisRAConstant RealText box -0.641RealSetThe right ascension of the body's spin axis at the orientation epoch.degOrientationEpoch G+SNone
53
CelestialBodySpinAxisRARate RealText box-0.641RealSetThe rate of change of the body's right ascension.deg/centuryNoneFRR-16.7.2G+SNone
54
CelestialBodyOrientationEpoch StringText box21545.06116.0 <= Epoch <= 58127.5SetThe reference epoch for orientation dataA1 Mod Julian EpochRotationConstant, RotationRate, SpinAxisDECConstant, SpinAxisDECRate, SpinAxisRAConstant, SpinAxisRARate FRR-16.7.7G+SNone
55
CelestialBodyPosVelSource StringDrop Down Menu''DE405' for build in bodies. 'SPICE' for user defined bodies.SPICE'SetThe model for the bodies orbit ephemeredes.GMAT currently only supports a single ephemeris model for custom bodies (SPICE) and this is set using PosVelSource field. The default for PosVelSource is SPICE and it is not necessary to configure this field in the current version of GMAT. This field has no effect for built-in bodies.N/ANoneFRR-16.3.0G+SNone
56
CelestialBodyRotationDataSource StringDrop Down MenuFor Earth default is 'FK5IAU1980', for Luna default is DE405, for selected build it bodies IAU2000, and for selected built in bodies and all user defined bodies, default is IAUSimplified.'IAUSimplified', 'DE405' 'FK5IAU1980', 'IAU2000'SetThe model for the body's time dependent orientation.N/ACoupling is based on body. See Default description.FRR-16.4.0G+SNone
57
CelestialBodyOrbitSpiceKernelNameStringArrayListN/AValid SPK kernelSetList of SPK kernels.N/ANoneFRR-16.6.1
58
CelestialBodyOrbitColor
Integer Array or String
ColorPickerOrchid for user-defined planet, Pink for user-defined Comet, Salmon for user-defined Asteriod, and Tan for user-defined MoonAny color available from the Target Color Picker in GUI. Valid predefined color name or RGB triplet value between 0 and 255.SetAllows you to set available colors on built-in or user-defined CelestialBody objects that are
drawn on the 3D OrbitView graphics displays. Colors on a CelestialBody object can be set
through a string or an integer array. For example: Setting a celestial body's orbit color to red can be done in the following
two ways: CelestialBody.OrbitColor = Red or Celestialbody.OrbitColor = [255 0 0]. This
field can be modified in the Mission Sequence as well.
N/AN/AG+SNone
59
CelestialBodyCentralBody UserDefStringDrop Down MenuFor Comet, Planet, Asteroid, the default is Sun. For Moon, the default is Earth.Celestial Body. SetThe central body of the celestial body. The central body field is used primarily by the GUI.N/ANoneFRR-16.8.10G+SNone
60
CelestialBodyTargetColor
Integer Array or String
ColorPickerDark gray for user-defined planet, Comet, Asteriod and MoonAny color available from the Target Color Picker in GUI. Valid predefined color name or RGB triplet value between 0 and 255.SetAllows you to select available colors for perturbing
CelestialBody orbital trajectories that are
drawn during iterative processes such as Differential Correction
or Optimization. The target color can be identified through a
string or an integer array. For example: Setting a celestial
body's perturbing trajectory color to yellow can be done in
following two ways: Celestialbody.TargetColor =
Yellow or Celestialbody.TargetColor = [255 255
0]. This field can be modified in the Mission Sequence
as well.
N/AN/AG+SNone
61
CelestialBodyNAIFId IntegerText Box-123456789IntegerSetNAIF Integer ID for body.N/APosVelSourceG+SNone
62
CoordinateSystem
Axes StringDrop Down MenuMJ2000EqMJ2000Eq, MJ2000Ec, ICRF, ITRF, MODEq, MODEc, TODEq, TODEc, MOEEq, MOEEc, TOEEq, TOEEc, ObjectReferenced, Equator, BodyFixed, BodyInertial, GSE, GSM, Topocentric, BodySpinSunSetThe axes of the coordinate system.N/AEpoch, Primary, Secondary, XAxis, YAxis, ZAxisFRR-35.2.0G + SNone
63
CoordinateSystem
EpochStringText Box21545See Epoch??SetThe reference epoch for the coordinate system. This field is only used for TOE amd MOE axis types.Modified Julian DateAxesFRR-35.2.3, FRR-35.2.4,
FRR-35.2.5, FRR-35.2.6
G+SNone
64
CoordinateSystem
PrimaryStringDrop Down MenuEarthCelestialBody, Spacecraft, LibrationPoint, Barycenter, SolarSystemBarycenter, GroundStationSetThe primary body for an ObjectReferenced axis system. This field is only use if Axes = ObjectReferenced.N/AAxesFRR-35.2.13G+SNone
65
CoordinateSystem
SecondaryStringDrop Down MenuLunaCelestialBody, Spacecraft, LibrationPoint, Barycenter, SolarSystemBarycenter, GroundStationSetThe secondary body for an ObjectReferenced axis system. This field is only use if Axes = ObjectReferenced.N/AAxesFRR-35.2.13G+SNone
66
CoordinateSystem
XAxisStringDrop Down MenuRR,V, N, -R, -V, -N, or emptySetThe x-axis definition for an ObjectReferenced axis system. This field is only use if Axes = ObjectReferenced.N/AAxesFRR-35.2.13G+SNone
67
CoordinateSystem
YAxisStringDrop Down MenuNo DefaultR,V, N, -R, -V, -N, or emptySetThe y-axis definition for an ObjectReferenced axis system. This field is only use if Axes = ObjectReferenced.N/AAxesFRR-35.2.13G+SNone
68
CoordinateSystem
ZaxisStringDrop Down MenuNR,V, N, -R, -V, -N, or emptySetThe z-axis for an ObjectReferenced axis system. This field is only use if Axes = ObjectReferenced.N/AAxesFRR-35.2.13G+SNone
69
CoordinateSystem
OriginUserDefStringDrop Down MenuEarthCelestialBody, Spacecraft, LibrationPoint, Barycenter, SolarSystemBarycenter, GroundStationSetThe origin of the coordinate system.N/ANoneFRR-35.1.0G+SNone
70
DataFileFilenameStringN/AEmpty stringN/Aset, getit specifies name of data fileN/ANoneS
71
DataFileFormatStringN/AGMATInternalGMATInternal, GMAT_OD, GMAT_ODDopler, GMAT_RampTableset, getit specifies data format of data fileN/ANoneS
72
DataFileDataThinningRatioRealN/A10 < number <= 1.0set, getit specifies ratio between number of picked records and total number of recordsno unitNoneS
73
DataFileSelectedStationIDsString ArrayN/Aempty listeach element in the list has to be a valid stationIDsset, getall data records with stationID is not in the list are throw away when GMAT read the data file. Special case: if the list is empty, all data records in data file are selected.N/AGroundStation's IDS
74
DataFileEpochFormatStringN/ATAIModJulian'all valid time typesetit specifies time format for time windowN/ADataFile's StartEpoch and EndEpochS
75
DataFileStartEpochStringN/A'6116'String containing time in range from 6116 TAIMJD to 58127.5 TAIMJDsetit specifies start epoch for time windowN/ADataFile's EpochFormat and EndEpochS
76
DataFileEndEpochStringN/A'58127.5'String containing time in range from 6116 TAIMJD to 58127.5 TAIMJDsetit specifies end epoch for time windowN/ADataFile's EpochFormat and StartEpochS
77
DifferentialCorrector
ReportFileFileNameText BoxDifferentialCorrectorDCName.data, where DCname is the name of the differential correctorFilename consistent with OS SetThe ReportFile field allows the user to specify the path and file name for the differential correction report.  The report is only generated if ShowProgress is set to true.  N/ANoneFRR-19.3G+SNone
78
DifferentialCorrector
MaximumIterationsIntegerText Box25Integer >= 1SetThe MaximumIterations field allows the user to set the maximum number of nominal passes the differential corrector is allowed to take during the attempt to find a solution. If the maximum iterations is reached, GMAT exits the target loop and continues to the next command in the mission
sequence. In this case, the objects retain their states as of the last nominal pass through the targeting loop.
N/ANoneFRR-19.1.1G+S-1
79
DifferentialCorrector
DerivativeMethodStringDrop Down MenuForwardDifferenceForwardDifference, BackwardDifference, CentralDifferenceSetThe DerivativeMethod field allows the user to choose between one-sided and central differencing for numerically determining the derivative.N/ANoneFRR-19.1.2.1-3G+SNone
80
DifferentialCorrector
ReportStyleStringDrop Down MenuNormalNormal, Concise, Verbose, DebugSetThe ReportStyle field allows the user to control the amount and type of information written to the file defined in the ReportFile field. Currently, the Normal and Concise options contain the same information: the Jacobian, the inverse of the Jacobian, the current values of the control variables, and achieved and desired values of the constraints. Verbose contains values of the perturbation variables in addition to the data for Normal and Concise. Debug contains detailed script snippets at each iteration for objects that have control variables.N/ANoneFRR-19.3G+SNone
81
DifferentialCorrector
ShowProgressStringCheckBoxtruetrue, falseSetWhen the ShowProgress field is set to true, then data illustrating the progress of the differential correction process are written to the message window and the ReportFile. The message window is updated with information on the current control variable values and the contraint variances.  When the ShowProgress field is set
to false, no information on the progress of the differential correction
process is displayed to the message window or written to the ReportFile.
N/ANoneFRR.19.2.1-3G+SNone
82
EphemerisFileInterpolationOrderIntegerTextBox7For CCSDS-OEM and Code 500 file formats: 1 <= Integer Number <= 10. For SPK file format:

1 <= Odd Integer Number <= 9

SetThe InterpolationOrder field allows you to set the interpolation order for the available interpolator methods (Lagrange or Hermite) for either CCSDS-OEM, SPK or Code 500-EPHEM file formats. N/ANoneFRR-31.4.4.1, FRR-31.5.4.1
G+SNone
83
EphemerisFileStepSizeRealTextBoxIntegratorStepsReal Number > 0.0 or equals 'IntegratorSteps'SetThe ephemeris file is generated at the step size that is specified for StepSize field. The user can generate ephemeris file at default Integration step size (using raw integrator steps) or by defining a Fixed step size provided by user. For Code 500 ephemeris, only fixed step size is supported.N/ANoneFRR-31.4.5G+SNone
84
EphemerisFileEpochFormatStringDropDownMenuUTCGregorianUTCGregorian, UTCModJulian, TAIGregorian, TAIModJulian, TTGregorian, TTModJulian A1Gregorian, A1ModJulian, TDBGregorian, TDBModJulianSetThe EpochFormat field allows the user to select format of the epoch.N/ANoneFRR-31.4.2, FRR-31.5.2
G+SNone
85
EphemerisFileFileFormatStringDropDownMenuCCSDS-OEMCCSDS-OEM, SPK, Code-500SetThe FileFormat field allows the user to generate ephemeris files in three available file formats: CCSDS-OEM, SPK and Code 500-EPHEMN/AInterpolatorFRR-31.2.0G+SNone
86
EphemerisFileFileNameStringTextBox, FileBrowseButtonEphemerisFile1.ephValid File Path and NameSetThe FileName field allows the user to name the generated ephemeris file and save it in user-specified location.N/ANoneFRR-31.19
G+SNone
87
EphemerisFileFinalEpochStringTextBoxFinalSpacecraftEpochuser-defined final epoch or 'FinalSpacecraftEpoch'SetThe FinalEpoch field allows the user to specify the time span of an ephemeris file. Ephemeris file is generated up to final epoch that is specified in FinalEpoch field.N/ANoneFRR-31.7.0G+SNone
88
EphemerisFileInitialEpochStringTextBoxInitialSpacecraftEpochuser-defined initial epoch or 'InitialSpacecraftEpoch'SetThe InitialEpoch field allows the user to specify the starting epoch of the ephemeris file.
Ephemeris file is generated starting from the epoch that is defined in InitialEpoch field.
N/ANoneFRR-31.7.0G+SNone
89
EphemerisFileInterpolatorStringDropDownMenuLagrangeLagrange for CCSDS and code 500-EPHEM file, Hermite for SPK fileSetThe Interpolator field defines the available interpolator method that was used to generate ephemeris file. Available Interpolators are Lagrange or Hermite.N/ANoneFRR-31.4.4.1
N/ANone
90
EphemerisFileOutputFormatStringDropDownMenuPCPC, UNIX, BigEndian, LittleEndianSetThe OutputFormat field allows the user to specify what type of format do they want to generate GSFC Code-500 ephemeris in. GSFC Code-500 ephemeris can be generated in the PC or UNIX version. N/AFileFormatG+S
91
EphemerisFileWriteEphemerisStringCheckBoxtruetrue,falseSetWriteEphemeris field allows the user to optionally calculate/write or not calculate/write an ephemeris that has been created and configured. N/ANoneFRR-31.10
G+SNone
92
EphemerisFileCoordinateSystemUserDefStringDropDownMenuEarthMJ2000EqAny default or user defined coordinate systemSet,GetCoordinateSystem field allows the user to generate ephemeris data in the coordinate system that is selected from CoordinateSystem field. The user can choose to also generate ephemeris data in user-defined coordinate system. N/ANoneFRR-31.4.3G+SNone
93
EphemerisFileSpacecraftUserDefStringDropDownMenuDefaultSCDefault spacecraft or any number of user-defined spacecrafts or formations Set,GetThe Spacecraft field allows the user to generate ephemeris data of spacecraft(s) that are defined in Spacecraft field.N/ANone FRR-31.1.0G+SNone
94
EphemerisFileUpperLeftStringN/A[ 0 0 ]Any Real numberSetThe UpperLeft field allows the user to pan the generated ephemeris file display
window in any direction. First value in [0 0] matrix helps to pan the
window horizontally and second value helps to pan the
window vertically.
N/ANoneFRR-31.18SNone
95
EphemerisFileSizeStringN/A[ 0 0 ]Any Real numberSetThe Size field allows the user to control the display size of generated ephemeris file panel. First value in [0 0] matrix controls horizonal
size and second value controls vertical size of ephemeris file display
window.
N/ANoneFRR-31.16SNone
96
EphemerisFileRelativeZOrderStringN/A0Any Real numberSetRelativeZOrder field allows the user to select which generated ephemeris file display window is to
displayed first on the screen. The EphemerisFile object with lowest
RelativeZOrder value will be displayed last while EphemerisFile object with
highest RelativeZOrder value will be displayed first.
N/ANoneFRR-31.17SNone
97
EphemerisFileMaximizedStringN/Afalsetrue,falseSetThe Maximized field allows the user to maximize the generated ephemeris file window.N/ANoneFRR-31.15SNone
98
ErrorModelTypeEnumerationN/ADSN_SeqRangeDSN_SeqRange, DSN_TCP, Range, RangeRate, GPS_PosVec, SN_Range, SN_DopplerSetMeasurement data typeN/AThe units on the fields, NoiseSigma and Bias, depend on the TypeFRR-47.2SNone
99
ErrorModelNoiseSigmaRealN/A103Re > 0SetOne sigma value of Gaussian noise. For simulations, if Sim.AddNoise= true, this noise is added to the measurements. For estimation, this value is used to as part of the batch processing algorithms. Range: km, DSN_SeqRange: RU, RangeRate: km/s, DSN_TCP: Hz, TDRSDoppler_HZ: HzThe units depend on the TypeFRR-47.3SNone
100
ErrorModelBiasRealN/A0Any Real numberSetThe constant bias associated with the measurement. For simulations, this bias is added to the measurement. Range: km, DSN_SeqRange: RU, RangeRate: km/s, DSN_TCP: Hz, TDRSDoppler_HZ: HzThe units depend on the TypeFRR-47.4SNoneIts default value has to be 0 (no bias)
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