FieldIntelsatElevenElementsPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total6 of 47198%0 of 0n/a217278217
getMass(FieldAbsoluteDate)30%n/a111111
getFrame()30%n/a111111
propagateInEcef(FieldAbsoluteDate)155100%n/a0102601
computeSatelliteEastLongitudeDegrees(FieldUnivariateDerivative2, FieldSinCos, FieldSinCos)98100%n/a0101301
computeSatelliteRadiusKilometers(CalculusFieldElement, FieldSinCos)52100%n/a0101101
FieldIntelsatElevenElementsPropagator(FieldIntelsatElevenElements, Frame, Frame, AttitudeProvider, CalculusFieldElement)48100%n/a0101001
computeSatelliteGeocentricLatitudeDegrees(FieldUnivariateDerivative2, FieldSinCos)34100%n/a010301
propagateOrbit(FieldAbsoluteDate, CalculusFieldElement[])24100%n/a010201
FieldIntelsatElevenElementsPropagator(FieldIntelsatElevenElements, Frame, Frame)16100%n/a010201
FieldIntelsatElevenElementsPropagator(FieldIntelsatElevenElements)10100%n/a010201
resetInitialState(FieldSpacecraftState)7100%n/a010101
resetIntermediateState(FieldSpacecraftState, boolean)7100%n/a010101
getEastLongitudeDegrees()3100%n/a010101
getGeocentricLatitudeDegrees()3100%n/a010101
getOrbitRadius()3100%n/a010101
getIntelsatElevenElements()3100%n/a010101
getParametersDrivers()2100%n/a010101