FieldEcksteinHechlerPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total31 of 91296%8 of 2263%9284141117
FieldEcksteinHechlerPropagator(FieldOrbit, RealFieldElement, double, double, double, double, double, double, double)130%n/a112211
computeMeanParameters(FieldCircularOrbit, RealFieldElement)1225295%61062%6913901
resetIntermediateState(FieldSpacecraftState, boolean)62076%1150%121601
toCartesian(FieldAbsoluteDate, FieldDerivativeStructure[])244100%n/a0103301
meanToEccentric(FieldDerivativeStructure, FieldDerivativeStructure, FieldDerivativeStructure)88100%1375%1301701
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, double, double, double, double, double, double, double)76100%n/a0101401
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics)30100%n/a010701
resetInitialState(FieldSpacecraftState)25100%n/a010501
propagateOrbit(FieldAbsoluteDate)21100%n/a010301
FieldEcksteinHechlerPropagator(FieldOrbit, double, double, double, double, double, double, double)20100%n/a010201
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, double, double, double, double, double, double, double)20100%n/a010201
FieldEcksteinHechlerPropagator(FieldOrbit, UnnormalizedSphericalHarmonicsProvider)19100%n/a010301
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider)19100%n/a010201
normalizeAngle(RealFieldElement, RealFieldElement)16100%n/a010101
FieldEcksteinHechlerPropagator(FieldOrbit, RealFieldElement, UnnormalizedSphericalHarmonicsProvider)12100%n/a010201
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, UnnormalizedSphericalHarmonicsProvider)12100%n/a010201
getMass(FieldAbsoluteDate)7100%n/a010101