TimeSpanParametricAcceleration

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total2 of 36199%2 of 3093%235175020
findByName(List, String)21890%1375%131501
extractParameters(CalculusFieldElement[], FieldAbsoluteDate)57100%6100%0401101
acceleration(FieldSpacecraftState, CalculusFieldElement[])55100%4100%030901
extractParameters(double[], AbsoluteDate)53100%6100%0401101
acceleration(SpacecraftState, double[])48100%4100%030901
getParametersDrivers()40100%1583%140701
TimeSpanParametricAcceleration(Vector3D, boolean, AttitudeProvider, AccelerationModel)18100%n/a010601
addAccelerationModelValidBefore(AccelerationModel, AbsoluteDate)8100%n/a010201
addAccelerationModelValidAfter(AccelerationModel, AbsoluteDate)8100%n/a010201
TimeSpanParametricAcceleration(Vector3D, boolean, AccelerationModel)7100%n/a010201
TimeSpanParametricAcceleration(Vector3D, AttitudeProvider, AccelerationModel)7100%n/a010201
init(SpacecraftState, AbsoluteDate)7100%n/a010201
getAccelerationModel(AbsoluteDate)6100%n/a010101
extractAccelerationModelRange(AbsoluteDate, AbsoluteDate)6100%n/a010101
getAccelerationModelSpan(AbsoluteDate)5100%n/a010101
lambda$init$0(SpacecraftState, AbsoluteDate, AccelerationModel)5100%n/a010101
getFirstSpan()4100%n/a010101
dependsOnPositionOnly()3100%n/a010101
getEventDetectors()2100%n/a010101
getFieldEventDetectors(Field)2100%n/a010101