ConstantThrustManeuver

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total15 of 55397%1 of 4897%1544125030
acceleration(FieldSpacecraftState, RealFieldElement[])93680%1375%1321001
ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D, String)69193%2100%0222201
init(SpacecraftState, AbsoluteDate)64100%16100%0901301
isFiring(AbsoluteDate)63100%18100%01001901
getFieldEventsDetectors(Field)40100%n/a010501
acceleration(SpacecraftState, double[])39100%4100%0301001
getEventsDetectors()32100%n/a010501
addContribution(FieldSpacecraftState, FieldTimeDerivativesEquations)22100%2100%020501
addContribution(SpacecraftState, TimeDerivativesEquations)19100%2100%020501
getISP()13100%n/a010301
getParametersDrivers()13100%n/a010101
ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D)10100%n/a010201
ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D, String)10100%n/a010201
ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D)9100%n/a010201
static {...}9100%n/a010201
lambda$getFieldEventsDetectors$3(FieldSpacecraftState, FieldDateDetector, boolean)7100%n/a010201
lambda$getFieldEventsDetectors$2(FieldSpacecraftState, FieldDateDetector, boolean)7100%n/a010201
getDuration()6100%n/a010101
isFiring(FieldSpacecraftState)6100%n/a010101
lambda$getEventsDetectors$1(SpacecraftState, DateDetector, boolean)6100%n/a010201
lambda$getEventsDetectors$0(SpacecraftState, DateDetector, boolean)6100%n/a010201
isFiring(SpacecraftState)5100%n/a010101
getThrust()4100%n/a010101
getFlowRate()4100%n/a010101
getDirection()3100%n/a010101
getName()3100%n/a010101
getStartDate()3100%n/a010101
getEndDate()3100%n/a010101
getAttitudeOverride()3100%n/a010101
dependsOnPositionOnly()2100%n/a010101