Serialized Form

Package talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.xmatch
- Class talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.xmatch.CloseEncounterElement extends java.lang.Object implements Serializable
  
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  1L
  - Serialized Fields
    - collision
      
      boolean collision
      
      Collision flag
    - distance
      
      double distance
      
      Minimum distance
    - endJD
      
      double endJD
      
      End of the close encounter
    - mainBody
      
      TARGET mainBody
      
      Main body
    - maxJD
      
      double maxJD
      
      Closest time of the encounter
    - ssoId
      
      java.lang.String ssoId
      
      SSO id
    - ssoName
      
      java.lang.String ssoName
      
      SSO name
    - ssoOid
      
      int ssoOid
      
      SSO oid
    - startJD
      
      double startJD
      
      Start of the close encounter
- Class talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.xmatch.CrossMatchElement extends java.lang.Object implements Serializable
  
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  - Serialized Fields
    - crossMatchAngDist
      
      float crossMatchAngDist
    - crossMatchDec
      
      double crossMatchDec
    - crossMatchEndJD
      
      double crossMatchEndJD
    - crossMatchJD
      
      double crossMatchJD
    - crossMatchMag
      
      java.lang.String crossMatchMag
    - crossMatchObsProb
      
      float crossMatchObsProb
    - crossMatchRa
      
      double crossMatchRa
    - crossMatchStartJD
      
      double crossMatchStartJD
    - crossMatchType
      
      int crossMatchType
    - ephemObsEnd
      
      DetailedEphemElement ephemObsEnd
    - ephemObsStart
      
      DetailedEphemElement ephemObsStart
    - image
      
      java.lang.String image
    - missionId
      
      java.lang.String missionId
    - obsEndJD
      
      double obsEndJD
    - observationId
      
      java.lang.String observationId
    - observationOid
      
      java.lang.String observationOid
    - obsPolygon
      
      java.lang.String obsPolygon
    - obsStartJD
      
      double obsStartJD
    - ssoId
      
      java.lang.String ssoId
    - ssoName
      
      java.lang.String ssoName
    - ssoOid
      
      int ssoOid
    - ssoType
      
      SSO_TYPE ssoType
Package talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem
- Class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.LocationElement extends java.lang.Object implements Serializable
  
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  - Serialized Fields
    - lonLatRad
      
      double[] lonLatRad
      
      Longitude, latitude, and radius.
    - xyz
      
      double[] xyz
      
      Rectangular vector.
- Class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.Matrix extends java.lang.Object implements Serializable
  
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  - Serialized Fields
    - data
      
      double[][] data
      
      Array for internal storage of elements.
      
      internal array storage.
    - m
      
      int m
      
      Row dimension
    - n
      
      int n
      
      Column dimension
- Class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.ObservatoryElement extends java.lang.Object implements Serializable
  
  serialVersionUID:
  
  1L
  - Serialized Fields
    - code
      
      java.lang.String code
      
      Observatory code
    - longitude
      
      double longitude
      
      Longitude
    - name
      
      java.lang.String name
      
      Observatory name
    - rhoCosLat
      
      double rhoCosLat
      
      Rho cos latitude
    - rhoSinLat
      
      double rhoSinLat
      
      Rho sine latitude
- Class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.OrbitalElement extends java.lang.Object implements Serializable
  
  serialVersionUID:
  
  1L
  - Serialized Fields
    - absoluteMagnitude
      
      float absoluteMagnitude
      
      Absolute magnitude.
    - argumentOfPerihelion
      
      double argumentOfPerihelion
      
      Argument of perihelion = longitude of perihelion - long. ascending node. Sometimes it is needed as a replacement to long. of perihelion. Radians.
    - ascendingNodeLongitude
      
      double ascendingNodeLongitude
      
      Ascending node longitude in radians.
    - ceu
      
      float ceu
      
      Uncertainty in position
    - ceuDate
      
      double ceuDate
      
      JD date of the reference uncertainty in position
    - ceuRate
      
      float ceuRate
      
      Rate of uncertainty in position
    - converge
      
      boolean converge
      
      Flag to set to false in case the elements refer to an hyperbolic orbit and the Kepler solution does not converge
    - eccentricity
      
      double eccentricity
      
      Eccentricity.
    - gravModel
      
      double[] gravModel
      
      Parameters for a non standard gravitational model, otherwise null. Values: ALN (.1112620426), NK (4.6142), NM (2.15), NN (5.093), R0 (2.808)
    - id
      
      java.lang.String id
      
      Object id;
    - inclination
      
      double inclination
      
      Inclination of orbit in radians.
    - magnitudeModel
      
      OrbitalElement.MAGNITUDE_MODEL magnitudeModel
      
      The magnitude model for the object.
    - magnitudeSlope
      
      float magnitudeSlope
      
      Magnitude slope for comets. Also used for CometPro magnitude model, parameter r.
    - magnitudeSlope2
      
      float magnitudeSlope2
      
      Magnitude slope 2 for comets. Used for CometPro magnitude model, parameter d.
    - maxMag
      
      double maxMag
      
      Maximum magnitude
    - meanAnomaly
      
      double meanAnomaly
      
      Mean anomaly = mean longitude - longitude of perihelion. Sometimes it is needed as a replacement to mean longitude. Radians.
    - meanLongitude
      
      double meanLongitude
      
      Mean longitude at reference time in radians.
    - meanMotion
      
      double meanMotion
      
      Mean motion in rad/day.
    - name
      
      java.lang.String name
      
      Name of the object.
    - ngfA
      
      double[] ngfA
      
      A1-A3 parameters of the standard non gravitational force referred to cometary jet forces (AU/s^2). Optional fourth parameter for the DT time offset, used in comets
    - orbitClass
      
      java.lang.String orbitClass
      
      Orbit classification
    - orbitCollisionStatus
      
      double orbitCollisionStatus
      
      Set to >0 to disable the calculations of cross matches with this body, with the value representing the Julian day of the collision of this body with another one. Also the preintegration is disabled when computing the initial conditions when this value is set to 0, to save speed, so the initial PV vector will not be accurate. Some constants defined in IntegratedBodyElement
    - perihelionDistance
      
      double perihelionDistance
      
      Perihelion distance in AU for comets.
    - perihelionLongitude
      
      double perihelionLongitude
      
      Perihelion longitude in radians.
    - perihelionTime
      
      double perihelionTime
      
      Reference date for the uncertainty in position
    - precalc
      
      OrbitalElement.Precalc precalc
      
      Precalculated quantities when solving the orbit
    - referenceEquinox
      
      double referenceEquinox
      
      Equinox of the orbital elements as a Julian day.
    - referenceTime
      
      double referenceTime
      
      Reference time as a Julian Day in TT . Usually perihelion time in comets.
    - semimajorAxis
      
      double semimajorAxis
      
      Semimajor axis of the orbit in AU.
- Class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.OrbitalElement.Precalc extends java.lang.Object implements Serializable
  
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  - Serialized Fields
    - m
      
      Matrix m
      
      Rotation matrix for precesion and orbit plane to ecliptic plane
    - oid
      
      int oid
      
      Oid of the body
    - posDifFromNGF
      
      double posDifFromNGF
      
      Position discrepancy in comets when parameters for NGF forces are used or not used
    - pvForRefTime
      
      double[] pvForRefTime
      
      Precalculated PV vector, ecliptic J2000, respect the Sun
    - tmp
      
      double tmp
      
      Stores Math.sqrt(Math.abs(1.0 - orbit.eccentricity * orbit.eccentricity)) to minimize recomputing the same square roots
    - tmp2
      
      double tmp2
      
      Stores 3.0 * Constants.EARTH_MEAN_ORBIT_RATE / (2.0 * q * FastMath.sqrt(2.0 * q)) for parabolic orbits, to minimize recomputing the same quantities
    - tmp3
      
      double tmp3
      
      Stores (1.0 - orbit.eccentricity) / (1.0 + orbit.eccentricity) for parabolic orbits, to minimize recomputing the same quantities
- Class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.Quadruple extends java.lang.Number implements Serializable
  
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  - Serialized Fields
    - exponent
      
      int exponent
      
      Exponent
    - mantHi
      
      long mantHi
      
      Mantissa high
    - mantLo
      
      long mantLo
      
      Mantissa low
    - negative
      
      boolean negative
      
      Negative flag
Package talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.moons
- Class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.moons.Complex extends java.lang.Object implements Serializable
  
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  - Serialized Fields
    - imaginary
      
      double imaginary
      
      Imaginary part.
    - real
      
      double real
      
      Real part.
- Class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.moons.MoonOrbitalElement extends java.lang.Object implements Serializable
  
  serialVersionUID:
  
  1L
  - Serialized Fields
    - absoluteMagnitude
      
      double absoluteMagnitude
      
      Absolute magnitude.
    - argumentOfPeriapsis
      
      double argumentOfPeriapsis
      
      Argument of periapsis = longitude of periapsis - long. ascending node. Sometimes it is needed as a replacement to long. of perihelion. Radians.
    - argumentOfPeriapsisPrecessionRate
      
      double argumentOfPeriapsisPrecessionRate
      
      Precession rate of the periapsis, rad/day.
    - ascendingNodeLongitude
      
      double ascendingNodeLongitude
      
      Ascending node longitude in radians.
    - ascendingNodePrecessionRate
      
      double ascendingNodePrecessionRate
      
      Precession rate of the ascending node, rad/day.
    - centralBody
      
      int centralBody
      
      Central body ID.
    - eccentricity
      
      double eccentricity
      
      Eccentricity.
    - inclination
      
      double inclination
      
      Inclination of orbit in radians.
    - laplacePoleDEC
      
      double laplacePoleDEC
      
      Declination of the local Laplace plane.
    - laplacePoleRA
      
      double laplacePoleRA
      
      Right ascension of the local Laplace plane.
    - magnitudeSlope
      
      double magnitudeSlope
      
      Magnitude slope.
    - meanAnomaly
      
      double meanAnomaly
      
      Mean anomaly = mean longitude - longitude of periapsis. Sometimes it is needed as a replacement to mean longitude. Radians.
    - meanLongitude
      
      double meanLongitude
      
      Mean longitude at reference time in radians.
    - meanMotion
      
      double meanMotion
      
      Mean motion in rad/day.
    - name
      
      java.lang.String name
      
      Name of the object.
    - periapsisDistance
      
      double periapsisDistance
      
      Perihelion distance in AU for comets.
    - periapsisLongitude
      
      double periapsisLongitude
      
      Perihelion longitude in radians.
    - preCalc
      
      MoonOrbitalElement.Precalc preCalc
      
      To precalculate some vectors.
    - referenceEphemeris
      
      java.lang.String referenceEphemeris
      
      Reference ephemeris.
    - referenceEquinox
      
      double referenceEquinox
      
      Equinox of the orbital elements as a Julian day.
    - referencePlane
      
      MoonOrbitalElement.REFERENCE_PLANE referencePlane
      
      Reference plane for the elements.
    - referenceTime
      
      double referenceTime
      
      Reference time in Julian Day. Usually perihelion time in comets.
    - semimajorAxis
      
      double semimajorAxis
      
      Semimajor axis of the orbit in AU.
- Class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.moons.MoonOrbitalElement.Precalc extends java.lang.Object implements Serializable
  
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  - Serialized Fields
    - avect
      
      double[] avect
      
      Vector a used in Rocks
    - bvect
      
      double[] bvect
      
      Vector b used in Rocks
    - cvect
      
      double[] cvect
      
      Vector c used in Rocks

Serialized Form

Package talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.xmatch

Class talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.xmatch.CloseEncounterElement extends java.lang.Object implements Serializable

Serialized Fields

collision

distance

endJD

mainBody

maxJD

ssoId

ssoName

ssoOid

startJD

Class talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.xmatch.CrossMatchElement extends java.lang.Object implements Serializable

Serialized Fields

crossMatchAngDist

crossMatchDec

crossMatchEndJD

crossMatchJD

crossMatchMag

crossMatchObsProb

crossMatchRa

crossMatchStartJD

crossMatchType

ephemObsEnd

ephemObsStart

image

missionId

obsEndJD

observationId

observationOid

obsPolygon

obsStartJD

ssoId

ssoName

ssoOid

ssoType

Package talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem

Class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.LocationElement extends java.lang.Object implements Serializable

Serialized Fields

lonLatRad

xyz

Class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.Matrix extends java.lang.Object implements Serializable

Serialized Fields

data

m

n

Class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.ObservatoryElement extends java.lang.Object implements Serializable

Serialized Fields

code

longitude

name

rhoCosLat

rhoSinLat

Class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.OrbitalElement extends java.lang.Object implements Serializable

Serialized Fields

absoluteMagnitude

argumentOfPerihelion

ascendingNodeLongitude

ceu

ceuDate

ceuRate

converge

eccentricity

gravModel

id

inclination

magnitudeModel

magnitudeSlope

magnitudeSlope2

maxMag

meanAnomaly

meanLongitude

meanMotion

name

ngfA

orbitClass

orbitCollisionStatus

perihelionDistance

perihelionLongitude