Package org.orekit.time
Enum Class GNSSDate.GNSSDateType
- All Implemented Interfaces:
Serializable,Comparable<GNSSDate.GNSSDateType>,Constable
- Enclosing class:
GNSSDate
Enumerate for GNSS data.
-
Nested Class Summary
Nested classes/interfaces inherited from class java.lang.Enum
Enum.EnumDesc<E extends Enum<E>> -
Enum Constant Summary
Enum Constants -
Method Summary
Modifier and TypeMethodDescriptionintGet the number of week in one rollover cycle.static intgetRollOverWeek(SatelliteSystem satellite) Get the number of week in one rollover cycle for the given satellite system.Get the satellite system.static GNSSDate.GNSSDateTypeReturns the enum constant of this class with the specified name.static GNSSDate.GNSSDateType[]values()Returns an array containing the constants of this enum class, in the order they are declared.
-
Enum Constant Details
-
GPS
GPS. -
GALILEO
Galileo. -
QZSS
QZSS. -
BEIDOU
BeiDou. -
NAVIC
NavIC. -
SBAS
SBAS.
-
-
Method Details
-
values
Returns an array containing the constants of this enum class, in the order they are declared.- Returns:
- an array containing the constants of this enum class, in the order they are declared
-
valueOf
Returns the enum constant of this class with the specified name. The string must match exactly an identifier used to declare an enum constant in this class. (Extraneous whitespace characters are not permitted.)- Parameters:
name- the name of the enum constant to be returned.- Returns:
- the enum constant with the specified name
- Throws:
IllegalArgumentException- if this enum class has no constant with the specified nameNullPointerException- if the argument is null
-
getRollOverCycle
public int getRollOverCycle()Get the number of week in one rollover cycle.- Returns:
- the number of week in one rollover cycle
-
getSatelliteSystem
Get the satellite system.- Returns:
- the satellite system
-
getRollOverWeek
Get the number of week in one rollover cycle for the given satellite system.- Parameters:
satellite- satellite system- Returns:
- the number of week in one rollover cycle for the given satellite system
-