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OBLATENESS - Enum in talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody
Enum to (de)activate the oblateness calculations.
OBLATENESS - Static variable in class talonsoalbi_at_gmail_dot_com.ssoxmatch.Constants
Value of the property OBLATENESS
ObservationElement - Class in talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.xmatch
Holds the information about an observation
ObservationElement(String, String, String, Double, Double, Double, Double, Double, String) - Constructor for class talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.xmatch.ObservationElement
Constructor for an observation
ObservationElement(String, String, String, String, String, Double, Double, Double, String) - Constructor for class talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.xmatch.ObservationElement
Constructor for an observation
ObservationGroupElement - Class in talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.xmatch
Holds the information about a group of similar observations, same mission, start/end times, and identical or very similar fovs.
ObservationGroupElement(ObservationElement) - Constructor for class talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.xmatch.ObservationGroupElement
Constructor for a single observation object
ObservatoryElement - Class in talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem
This is a convenience class holding the data for the IAU list of observatories.
ObservatoryElement(String, String, double, double, double) - Constructor for class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.ObservatoryElement
Main constructor
ObsListService - Class in talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.web
 
ObsListService() - Constructor for class talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.web.ObsListService
 
Oceana - talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody.TARGET
Oceana
Octavia - talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody.TARGET
Octavia
ODE_SOLVER - Enum in talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody
Options for different ODE solvers (aka Runge-Kutta schemes) to apply.
ODE_SOLVER - Static variable in class talonsoalbi_at_gmail_dot_com.ssoxmatch.Constants
Value of the property ODE_SOLVER
OFF - talonsoalbi_at_gmail_dot_com.ssoxmatch.Main.LOG_LEVEL
No logs
Olga - talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody.TARGET
Olga
one() - Static method in class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.Quadruple
Returns a new Quadruple instance with the value of 1.0.
ONLY_EARTH_MOON_AND_MERCURY_PER_11_ITER - talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody.USE_JPL_FOR_PLANETS
Correct Earth, Moon, and Mercury (and the Sun) every 11 iterations
ONLY_EARTH_MOON_AND_MERCURY_PER_5_ITER - talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody.USE_JPL_FOR_PLANETS
Correct Earth, Moon, and Mercury (and the Sun) every 5 iterations
ONLY_EARTH_MOON_PER_5_ITER - talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody.USE_JPL_FOR_PLANETS
Correct Earth and Moon (and the Sun) every 5 iterations
ONLY_J2_EARTH - talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody.OBLATENESS
Accurate mode, but restricted to the J2 term of Earth
ONLY_MERCURY_ALL_ITERATIONS - talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody.USE_JPL_FOR_PLANETS
Correct Mercury (and the Sun) in every iteration
ONLY_MERCURY_PER_11_ITER - talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody.USE_JPL_FOR_PLANETS
Correct only Mercury (and the Sun) every 11 iterations
ONLY_MERCURY_PER_5_ITER - talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody.USE_JPL_FOR_PLANETS
Correct only Mercury (and the Sun) every 5 iterations
ONLY_SUN_ALL_ITERATIONS - talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody.USE_JPL_FOR_PLANETS
Correct only the Sun in every iteration
ONO_1210 - talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody.ODE_SOLVER
R12(10).
Ophelia - talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody.TARGET
Ophelia
OrbitalElement - Class in talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem
An adequate class for storing orbital elements.
OrbitalElement() - Constructor for class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.OrbitalElement
Constructs an empty OrbitalElement object.
OrbitalElement(String, String, double, double, double, double, double, double, double, double, double, double, double, double, float, float, OrbitalElement.MAGNITUDE_MODEL) - Constructor for class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.OrbitalElement
Constructs an OrbitalElement object giving the values of all the fields except the frame, which is FK5.
OrbitalElement(String, String, double, double, double, double, double, double, double, double, double, OrbitalElement.MAGNITUDE_MODEL) - Constructor for class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.OrbitalElement
Constructs an OrbitalElement object giving the values of most of the fields, but in a different way sometimes used.
OrbitalElement.MAGNITUDE_MODEL - Enum in talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem
The different magnitude models for comets and asteroids.
OrbitalElement.Precalc - Class in talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem
Little class to hold precalculated values to speed up the computation or the orbits
OrbitEphem - Class in talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem
Main class to compute ephemerides for minor bodies, solving their orbits for a given date from their orbital elements
orbitPlane(OrbitalElement, double) - Static method in class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.OrbitEphem
Obtain rectangular coordinates of the object in the orbit plane, according to the object's orbit: elliptic, parabolic, or hyperbolic.
orbitPlaneToEcliptic(OrbitalElement, double) - Static method in class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.OrbitEphem
Fast computation of ecliptic J2000 coordinates for an asteroid or comet.
orbitPlaneToEquator(OrbitalElement, double) - Static method in class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.OrbitEphem
Fast computation of equatorial J2000 coordinates for an asteroid or comet.
orbitPlaneToEquatorFromSat(OrbitalElement, double, double[]) - Static method in class talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.OrbitEphem
Fast computation of astrometric J2000 satellite-centric equatorial coordinates for an asteroid or comet.
orbitPlaneToEquatorFromSat(OrbitalElement, double, double[], boolean, double) - Static method in class talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.xmatch.ComputeAndIngest
Compute the position of a body respect the position vector of a given satellite.
orbitPlaneToEquatorFromSatIntegrate(OrbitalElement, double, double[], int) - Static method in class talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.xmatch.ComputeAndIngest
Compute the position of a body respect the position vector of a given satellite, forcing the use of numerical integration
Ornamenta - talonsoalbi_at_gmail_dot_com.ssoxmatch.ephem.nbody.TARGET
Ornamenta
overFootprint(double, double, BufferedImage) - Static method in class talonsoalbi_at_gmail_dot_com.ssoxmatch.actions.xmatch.ObservationElement
Returns if a given position lies inside the footprint according to pixel color.
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