normalizeAngle(RealFieldElement, RealFieldElement) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates, Frame, RealFieldElement) | | 97% | | 75% | 1 | 3 | 2 | 58 | 0 | 1 |
FieldEquinoctialOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, RealFieldElement) | | 94% | | 83% | 2 | 9 | 2 | 43 | 0 | 1 |
addKeplerContribution(PositionAngle, RealFieldElement, RealFieldElement[]) | | 96% | | 75% | 1 | 4 | 1 | 14 | 0 | 1 |
computeJacobianMeanWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 57 | 0 | 1 |
computePVWithoutA() | | 100% | | 100% | 0 | 2 | 0 | 34 | 0 | 1 |
interpolate(FieldAbsoluteDate, Stream) | | 100% | | 100% | 0 | 7 | 0 | 39 | 0 | 1 |
nonKeplerianAcceleration() | | 100% | | n/a | 0 | 1 | 0 | 22 | 0 | 1 |
computeJacobianTrueWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 23 | 0 | 1 |
shiftedBy(RealFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 17 | 0 | 1 |
meanToEccentric(RealFieldElement, RealFieldElement, RealFieldElement) | | 100% | | 75% | 1 | 3 | 0 | 17 | 0 | 1 |
toOrbit() | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
computeJacobianEccentricWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
FieldEquinoctialOrbit(FieldOrbit) | | 100% | | n/a | 0 | 1 | 0 | 17 | 0 | 1 |
eccentricToTrue(RealFieldElement, RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
trueToEccentric(RealFieldElement, RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
initPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
toString() | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
getIDot() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
getLMDot() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
getLEDot() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
getEDot() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
FieldEquinoctialOrbit(RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, RealFieldElement, PositionAngle, Frame, FieldAbsoluteDate, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getL(PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
getLDot(PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
eccentricToMean(RealFieldElement, RealFieldElement, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLM() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
shiftedBy(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
FieldEquinoctialOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getLE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
hasDerivatives() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getADot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialExDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEyDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHxDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHyDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLvDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |