FieldKeplerianPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total15 of 26194%2 of 1485%218254011
fixState(FieldOrbit, FieldAttitude, CalculusFieldElement, CalculusFieldElement, FieldArrayDictionary, FieldArrayDictionary)126584%1787%1521501
resetInitialState(FieldSpacecraftState)33592%1150%1201001
FieldKeplerianPropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement, CalculusFieldElement)35100%n/a010801
propagateOrbit(FieldAbsoluteDate, CalculusFieldElement[])21100%2100%020401
resetIntermediateState(FieldSpacecraftState, boolean)19100%2100%020501
FieldKeplerianPropagator(FieldOrbit)17100%n/a010301
FieldKeplerianPropagator(FieldOrbit, CalculusFieldElement)16100%n/a010301
FieldKeplerianPropagator(FieldOrbit, AttitudeProvider)15100%n/a010201
FieldKeplerianPropagator(FieldOrbit, AttitudeProvider, CalculusFieldElement)14100%n/a010201
getMass(FieldAbsoluteDate)7100%n/a010101
getParametersDrivers()2100%n/a010101