Maneuver

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total9 of 28396%2 of 1485%226263019
acceleration(FieldSpacecraftState, CalculusFieldElement[])93076%1375%132801
acceleration(SpacecraftState, double[])36100%4100%030801
getParametersDrivers()33100%n/a010801
addContribution(FieldSpacecraftState, FieldTimeDerivativesEquations)31100%2100%020501
addContribution(SpacecraftState, TimeDerivativesEquations)28100%2100%020501
getManeuverTriggersParameters(CalculusFieldElement[])16100%n/a010301
getManeuverTriggersParameters(double[])15100%n/a010301
getName()14100%1150%120401
Maneuver(AttitudeProvider, ManeuverTriggers, PropulsionModel)12100%n/a010501
init(SpacecraftState, AbsoluteDate)11100%n/a010301
init(FieldSpacecraftState, FieldAbsoluteDate)11100%n/a010301
getPropulsionModelParameters(CalculusFieldElement[])9100%n/a010101
getPropulsionModelParameters(double[])8100%n/a010101
getFieldEventsDetectors(Field)5100%n/a010101
getEventsDetectors()4100%n/a010101
getAttitudeOverride()3100%n/a010101
getPropulsionModel()3100%n/a010101
getManeuverTriggers()3100%n/a010101
dependsOnPositionOnly()2100%n/a010101