TimeStampedAngularCoordinates orientation
Frame referenceFrame
TimeSpanMap<T> activated
List<E extends Object> switches
Ellipsoid ellipsoid
Frame celestialFrame
CelestialBodyPointed.phasingCel
is defined.Vector3D phasingCel
Vector3D phasingSat
PVCoordinatesProvider pointedBody
Vector3D pointingSat
Attitude referenceAttitude
Frame satelliteFrame
AttitudeProvider attitudeLaw
Vector3D satPointingVector
BodyShape shape
BodyShape shape
Vector3D axis
AttitudeProvider nonRotatingLaw
double rate
Vector3D spin
AbsoluteDate start
private Object writeReplace() throws NotSerializableException
NotSerializableException
- if the state mapper cannot be serialized (typically for DSST propagator)AngularDerivativesFilter filter
Frame inertialFrame
LOFType type
private Object writeReplace() throws NotSerializableException
NotSerializableException
- if the state mapper cannot be serialized (typically for DSST propagator)AngularDerivativesFilter filter
Frame referenceFrame
Vector3D target
GroundPointing groundPointingLaw
GroundPointing groundPointingLaw
PVCoordinates phasingNormal
PVCoordinatesProvider sun
double a
double a2
double b
double b2
Vector3D center
double e2
double evoluteFactorX
double evoluteFactorY
Frame frame
double g
double g2
Vector3D u
Vector3D v
double a
double b
double c
Frame frame
RealFieldElement<T extends Object> altitude
RealFieldElement<T extends Object> latitude
RealFieldElement<T extends Object> longitude
double altitude
double latitude
double longitude
private Object writeReplace()
This intermediate class serializes the files supported names, the ephemeris type and the body name.
double ae2
double angularThreshold
double ap2
Frame bodyFrame
double e2
double f
double g
double g2
double lE
double lEDot
double lJu
double lJuDot
double lMa
double lMaDot
double lMe
double lMeDot
double lNe
double lNeDot
double lSa
double lSaDot
double lUr
double lUrDot
double lVe
double lVeDot
double pa
double paDot
double d
AbsoluteDate date
double dDot
double f
double fDot
double gamma
double gammaDot
double l
double lDot
double lPrime
double lPrimeDot
double omega
double omegaDot
double tc
private Object writeReplace()
This intermediate class serializes only the frame key.
IERSConventions conventions
double[] dCoefficients
double[] fCoefficients
double[] lCoefficients
double[] lECoefficients
double[] lJCoefficients
double[] lMaCoefficients
double[] lMeCoefficients
double[] lNeCoefficients
double[] lPrimeCoefficients
double[] lSaCoefficients
double[] lUCoefficients
double[] lVeCoefficients
double[] omegaCoefficients
double[] paCoefficients
TimeScale timeScale
double[] coefficients
Object[] parts
Localizable specifier
OrekitException wrappedException
Object[] parts
Localizable specifier
Object[] parts
Localizable specifier
String[] parts
Localizable specifier
Object[] parts
Localizable specifier
Object[] parts
Localizable specifier
double clock
double clockRate
BodyShape earth
DTM2000InputParameters inputParams
PVCoordinatesProvider sun
OneAxisEllipsoid earth
double n
PVCoordinatesProvider sun
double[][] tabAltRho
BodyShape earth
JB2008InputParameters inputParams
PVCoordinatesProvider sun
BodyShape earth
NRLMSISE00InputParameters inputParams
PVCoordinatesProvider sun
int[] sw
int[] swc
double h0
double hscale
double rho0
BodyShape shape
org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation.LineParameters currentParam
SortedSet<E extends Object> data
Pattern dataPattern
AbsoluteDate firstDate
AbsoluteDate lastDate
org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation.LineParameters previousParam
MarshallSolarActivityFutureEstimation.StrengthLevel strengthLevel
String supportedNames
AttitudeProvider attitudeOverride
Vector3D deltaVSat
boolean forward
double isp
EventDetector trigger
double vExhaust
private Object writeReplace()
This intermediate class serializes only the frame key.
IERSConventions conventions
AbsoluteDate date
double ddEps
double ddPsi
double dt
double dx
double dy
ITRFVersion itrfType
double lod
int mjd
double x
double y
private Object writeReplace()
This intermediate class serializes only the frame key.
IERSConventions conventions
boolean hasData
EOPHistory.hasDataFor(AbsoluteDate)
private Object writeReplace()
This intermediate class serializes only the frame key.
Predefined factoryKey
int depth
String name
Frame parent
boolean pseudoInertial
TransformProvider transformProvider
private Object writeReplace()
This intermediate class serializes only the frame key.
IERSConventions conventions
EOPHistory eopHistory
PVCoordinates cartesian
AbsoluteDate epoch
Vector3D rotationRate
Vector3D rotationVector
private Object writeReplace()
This intermediate class serializes only the data needed for generation, but does not serializes the cache itself (in fact the cache is not serializable).
AngularDerivativesFilter aFilter
CartesianDerivativesFilter cFilter
TransformProvider rawProvider
double step
ITRFVersion destination
ITRFVersion origin
TransformProvider provider
Frame frame
CelestialBody primaryBody
CelestialBody secondaryBody
List<E extends Object> children
Frame frame
String name
OrphanFrame orphanParent
TransformProvider provider
boolean pseudoInertial
double xp
double yp
private Object writeReplace()
This intermediate class serializes only the data needed for generation, but does not serializes the cache itself (in fact the cache is not serializable).
InterpolatingTransformProvider interpolatingProvider
BodyShape parentShape
GeodeticPoint point
AngularCoordinates angular
PVCoordinates cartesian
AbsoluteDate date
Frame inertialFrame
ExtendedPVCoordinatesProvider sun
AbsoluteDate validityEnd
AbsoluteDate validityStart
double END_MARGIN
double END_MARGIN
double yawRate
double END_MARGIN
double END_MARGIN
double altitude
double elev_star
double refrac_star
double theta0
double thetamin
double correfrac
double pressure
double temperature
private Object readResolve()
double[][] fArr
double[] xArr
double[] yArr
AbsoluteDate defaultDate
Geoid.harmonics
. Used when
no other dates are available. Should be removed in a future release.ReferenceEllipsoid referenceEllipsoid
Vector3D b
double declination
double horizontalIntensity
double inclination
double totalIntensity
double[] alpha
double[] beta
double ratio
double e0
double lambda
double latitude
double P0
double T0
double GM
double spin
private Object writeReplace()
double p0
double r0
double t0
GeodeticPoint v0
GeodeticPoint v1
GeodeticPoint v2
GeodeticPoint v3
private Object writeReplace()
double a
double aDot
double alphaV
double alphaVDot
double ex
double exDot
double ey
double eyDot
double i
double iDot
double raan
double raanDot
boolean serializePV
PVCoordinates
serialization.private Object writeReplace()
double a
double aDot
double ex
double exDot
double ey
double eyDot
double hx
double hxDot
double hy
double hyDot
double lv
double lvDot
private Object writeReplace()
double a
double aDot
double e
double eDot
double i
double iDot
double pa
double paDot
double raan
double raanDot
double v
double vDot
AbsoluteDate date
Frame frame
double mu
private Object writeReplace()
private Object writeReplace() throws NotSerializableException
NotSerializableException
- if an additional state provider is not serializabledouble[] ck0
org.orekit.propagation.analytical.EcksteinHechlerPropagator.EHModel initialModel
double mu
double referenceRadius
private Object writeReplace()
This intermediate class serializes only the data needed for generation, but does not serializes the cache itself (in fact the cache is not serializable).
String[] additional
double extrapolationThreshold
Frame frame
AbsoluteDate maxDate
AbsoluteDate minDate
org.orekit.propagation.analytical.Ephemeris.LocalPVProvider pvProvider
private Object writeReplace() throws NotSerializableException
NotSerializableException
- if an additional state provider is not serializableSpacecraftState initialState
double bStar
char classification
double eccentricity
int elementNumber
int ephemerisType
AbsoluteDate epoch
double inclination
int launchNumber
String launchPiece
int launchYear
String line1
String line2
double meanAnomaly
double meanMotion
double meanMotionFirstDerivative
double meanMotionSecondDerivative
double pa
double raan
int revolutionNumberAtEpoch
int satelliteNumber
boolean forward
EventHandler<T extends EventDetector> handler
double maxCheck
int maxIter
double threshold
double alignAngle
PVCoordinatesProvider body
double cosAlignAngle
double sinAlignAngle
double altitude
BodyShape bodyShape
PVCoordinatesProvider beacon
PVCoordinatesProvider observer
double proximityAngle
Vector3D center
double halfAperture
PVCoordinatesProvider targetPVProvider
int currentIndex
ArrayList<E extends Object> eventDateList
AbsoluteDate gDate
PVCoordinatesProvider occulted
double occultedRadius
PVCoordinatesProvider occulting
double occultingRadius
boolean totalEclipse
ElevationMask elevationMask
double minElevation
AtmosphericRefractionModel refractionModel
TopocentricFrame topo
TopocentricFrame topo
private Object writeReplace() throws NotSerializableException
NotSerializableException
- if the enabling predicate
is not serializableEventDetector rawDetector
double decreasingOffset
EventDetector detector
double increasingOffset
boolean useShiftedStates
EventDetector detector
boolean increasing
SpacecraftState state
AbsoluteDate extremeT
FilterType filter
boolean forward
EventDetector rawDetector
org.orekit.propagation.events.Transformer[] transformers
AbsoluteDate[] updates
AbsoluteDate afterEvent
double afterG
EventDetector detector
AbsoluteDate earliestTimeConsidered
boolean forward
double g0
boolean g0Positive
boolean increasing
double lastG
AbsoluteDate lastT
boolean pendingEvent
AbsoluteDate pendingEventTime
AbsoluteDate stopTime
AbsoluteDate t0
private Object writeReplace()
double margin
FieldOfView fov
PVCoordinatesProvider targetPVProvider
private Object writeReplace()
OneAxisEllipsoid body
double samplingStep
FunctionalDetector.GFunction gFunction
FieldOfView fov
Frame frame
OneAxisEllipsoid body
double latitude
OneAxisEllipsoid body
OneAxisEllipsoid body
double longitude
double previousDelta
double sign
OneAxisEllipsoid body
EventDetector original
Frame frame
double angle
OrbitType orbitType
PositionAngle positionAngle
double previousDelta
double sign
private Object writeReplace() throws NotSerializableException
NotSerializableException
- if the state mapper cannot be serialized (typically for DSST propagator)StateMapper mapper
AbsoluteDate maxDate
boolean meanOrbit
This is used only in the case of semianalitical propagators where there is a clear separation between mean and short periodic elements. It is ignored by the Numerical propagator.
AbsoluteDate minDate
DenseOutputModel model
AbsoluteDate startDate
Map<K extends Object,V extends Object> unmanaged
ArrayList<E extends Object> abscissae
int interpolationPoints
int latestClosestNeighbor
ArrayList<E extends Object> values
long epoch
Beware, it is not AbsoluteDate.J2000_EPOCH
since it is in TAI and not in TT.
double offset
int day
int month
int year
DateComponents date
TimeComponents time
UTCScale utc
AbsoluteDate referenceDate
UT1Scale ut1
TDBScale tdb
int hour
int minute
int minutesFromUTC
Always an integral number of minutes, as per ISO-8601 standard.
double second
EOPHistory eopHistory
UTCScale utc
private Object writeReplace()
org.orekit.time.UTCTAIOffset[] offsets
double[][] azelmask
double[][] imaginary
double[][] plus
double[][] real
double[] cuts
boolean[] flags
int[] leafs
double tolerance
AbsoluteDate date
private Object writeReplace()
AbsoluteDate date
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