ConstantThrustManeuver

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total40 of 47391%3 of 3892%9461198627
acceleration(FieldSpacecraftState, RealFieldElement[])93579%1375%1321001
ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D, String)68893%2100%0222101
getDuration()60%n/a111111
getDirection()30%n/a111111
getName()30%n/a111111
getStartDate()30%n/a111111
getEndDate()30%n/a111111
getAttitudeOverride()30%n/a111111
acceleration(SpacecraftState, double[])23694%1375%1311001
lambda$getFieldEventsDetectors$3(FieldSpacecraftState, FieldDateDetector, boolean)2880%1150%120201
init(SpacecraftState, AbsoluteDate)59100%20100%0110801
getFieldEventsDetectors(Field)40100%n/a010501
getEventsDetectors()32100%n/a010501
addContribution(FieldSpacecraftState, FieldTimeDerivativesEquations)21100%2100%020501
addContribution(SpacecraftState, TimeDerivativesEquations)18100%2100%020501
getISP()13100%n/a010301
getParametersDrivers()13100%n/a010101
ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D)10100%n/a010201
ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D, String)10100%n/a010201
lambda$getEventsDetectors$1(SpacecraftState, DateDetector, boolean)10100%2100%020201
ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D)9100%n/a010201
static {...}9100%n/a010201
lambda$getFieldEventsDetectors$2(FieldSpacecraftState, FieldDateDetector, boolean)6100%n/a010201
lambda$getEventsDetectors$0(SpacecraftState, DateDetector, boolean)6100%n/a010201
getThrust()4100%n/a010101
getFlowRate()4100%n/a010101
dependsOnPositionOnly()2100%n/a010101