GroundStation(TopocentricFrame, EOPHistory, StationDisplacement[]) | | 95% | | 75% | 1 | 3 | 1 | 21 | 0 | 1 |
getOffsetGeodeticPoint(AbsoluteDate) | | 85% | | 50% | 1 | 2 | 1 | 10 | 0 | 1 |
getEstimatedUT1() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
getOffsetToInertial(Frame, FieldAbsoluteDate, int, Map) | | 100% | | n/a | 0 | 1 | 0 | 19 | 0 | 1 |
getOffsetToInertial(Frame, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 16 | 0 | 1 |
computeDisplacement(AbsoluteDate, Vector3D) | | 100% | | 100% | 0 | 3 | 0 | 6 | 0 | 1 |
getOffsetToInertial(Frame, AbsoluteDate, int, Map) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
static {...} | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
GroundStation(TopocentricFrame) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getDisplacements() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPrimeMeridianOffsetDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPrimeMeridianDriftDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPolarOffsetXDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPolarDriftXDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPolarOffsetYDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPolarDriftYDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getClockOffsetDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getClockDriftDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEastOffsetDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getNorthOffsetDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getZenithOffsetDriver() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getBaseFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEstimatedEarthFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |