meanToHyperbolicEccentric(RealFieldElement, RealFieldElement) | | 92% | | 87% | 2 | 9 | 2 | 23 | 0 | 1 |
meanToEccentric(RealFieldElement, RealFieldElement, RealFieldElement) | | 92% | | 75% | 1 | 3 | 1 | 16 | 0 | 1 |
shiftPVElliptic(RealFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 42 | 0 | 1 |
shiftPVHyperbolic(RealFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 41 | 0 | 1 |
addKeplerContribution(PositionAngle, double, RealFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
getE() | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
getHxDot() | | 100% | | 83% | 1 | 4 | 0 | 11 | 0 | 1 |
getHyDot() | | 100% | | 83% | 1 | 4 | 0 | 11 | 0 | 1 |
getEDot() | | 100% | | 100% | 0 | 2 | 0 | 12 | 0 | 1 |
FieldCartesianOrbit(FieldOrbit) | | 100% | | 100% | 0 | 4 | 0 | 13 | 0 | 1 |
getPositionDS() | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
getVelocityDS() | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
FieldCartesianOrbit(TimeStampedFieldPVCoordinates, Frame, double) | | 100% | | 100% | 0 | 2 | 0 | 9 | 0 | 1 |
getHx() | | 100% | | 75% | 1 | 3 | 0 | 7 | 0 | 1 |
getHy() | | 100% | | 75% | 1 | 3 | 0 | 7 | 0 | 1 |
initEquinoctial() | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
toOrbit() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
getADot() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
create6x6Identity() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
getA() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
shiftedBy(RealFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
getIDot() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
interpolate(FieldAbsoluteDate, Stream) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
shiftedBy(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
toString() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
FieldCartesianOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEquinoctialExDot() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEquinoctialEyDot() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getLv() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getLvDot() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getLE() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getLEDot() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getLM() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getLMDot() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
static {...} | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
hasDerivatives() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
initPVCoordinates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
computeJacobianMeanWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
computeJacobianEccentricWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
computeJacobianTrueWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
lambda$interpolate$0(FieldOrbit) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |