FieldGnssOrbitalElements(CalculusFieldElement, double, int, TimeScales, SatelliteSystem) |  | 0% | | n/a | 1 | 1 | 9 | 9 | 1 | 1 |
FieldGnssOrbitalElements(Field, GNSSOrbitalElements) |  | 100% | | n/a | 0 | 1 | 0 | 23 | 0 | 1 |
FieldGnssOrbitalElements(Function, FieldGnssOrbitalElements) |  | 100% | | n/a | 0 | 1 | 0 | 23 | 0 | 1 |
getMeanMotion0() |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setGnssDate(GNSSDate) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getADot() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDeltaN0() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDeltaN0Dot() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setSma(CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setE(CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setI0(CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setOmega0(CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setPa(CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setM0(CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getDate() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMu() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getSma() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getE() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI0() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getOmega0() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPa() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getM0() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |