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Jeospace API | ||||||||||
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| Packages that use Epoch | |
| org.jeospace.physics.orbit | Contains interfaces and classes supporting physics based orbital mechanics. |
| org.jeospace.simulation | Contains classes to configure, manage and control the simulation/visulation environment. |
| org.jeospace.text | Contains classes for handling the textual representation of measurement and identity objects |
| Uses of Epoch in org.jeospace.physics.orbit |
| Fields in org.jeospace.physics.orbit declared as Epoch | |
static Epoch |
Epoch.B1900
The epoch B1900 |
static Epoch |
Epoch.B1950
The epoch B1950 |
static Epoch |
Epoch.J2000
The epoch J2000 |
static Epoch |
Epoch.J2050
The epoch J2050 |
static Epoch |
Epoch.MJD
The epoch of the Modified Julian day |
| Methods in org.jeospace.physics.orbit that return Epoch | |
Epoch |
OrbitalElements.getTimeOfPeriapsis()
Return the Julian Day of the time of periapsis |
Epoch |
OrbitalElements.getEpoch()
Return the epoch |
| Methods in org.jeospace.physics.orbit with parameters of type Epoch | |
int |
Epoch.compareTo(Epoch that)
Compare this object with the argument for order. |
| Constructors in org.jeospace.physics.orbit with parameters of type Epoch | |
OrbitalElements(double eccentricity,
Longitude inclination,
Longitude ascendingNode,
Longitude argumentOfPeriapsis,
Length distanceOfPeriapsis,
Epoch timeOfPeriapsis,
Epoch epoch,
double GM)
Create an OrbitalElements object with the given parameters. |
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OrbitalElements(double eccentricity,
Longitude inclination,
Longitude ascendingNode,
Longitude argumentOfPeriapsis,
Length semiMajorAxis,
Longitude meanAnomalyAtTheEpoch,
Epoch epoch,
double GM)
Create an OrbitalElements object with the given parameters. |
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OrbitalElements(double eccentricity,
Longitude inclination,
Longitude ascendingNode,
Longitude argumentOfPeriapsis,
Longitude meanAnomalyAtTheEpoch,
DecimalAngle meanMotion,
double dragCoefficient,
Epoch epoch,
double GM)
Create an OrbitalElements object with the given parameters. |
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Epoch(Epoch epoch)
Construct an Epoch object initialized to the value of the
argument. |
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| Uses of Epoch in org.jeospace.simulation |
| Methods in org.jeospace.simulation that return Epoch | |
Epoch |
Unmarshal.getEpoch(org.w3c.dom.Element epoch_element)
Return the Epoch that cooresponds to the argument |
| Methods in org.jeospace.simulation with parameters of type Epoch | |
org.w3c.dom.Element |
Marshal.createEpoch(java.lang.String tag,
Epoch epoch)
Create and return an Element cooresponding to the argument
Epoch object |
org.w3c.dom.Element |
Marshal.createEpoch(java.lang.String tag,
EpochFormatStyle style,
Epoch epoch)
Create and return an Element cooresponding to the argument
Epoch object |
| Uses of Epoch in org.jeospace.text |
| Methods in org.jeospace.text that return Epoch | |
Epoch |
EpochFormat.parse(java.lang.String value)
Return the Epoch that cooresponds to the argument value |
| Methods in org.jeospace.text with parameters of type Epoch | |
java.lang.String |
EpochFormat.format(Epoch epoch)
Return the String for the Epoch |
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Jeospace API | ||||||||||
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