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