BoxAndSolarArraySpacecraft

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total24 of 1,28298%0 of 50100%0528191027
buildDragParameterDriver(double)61062%n/a012301
buildLiftParameterDriver(double)61062%n/a012301
buildAbsorptionParameterDriver(double)61062%n/a012301
buildReflectionParameterDriver(double)61062%n/a012301
dragAcceleration(FieldAbsoluteDate, Frame, FieldVector3D, FieldRotation, RealFieldElement, RealFieldElement, FieldVector3D, RealFieldElement[])155100%6100%0402301
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[])122100%6100%0401901
getNormal(AbsoluteDate, Frame, FieldVector3D, FieldRotation)97100%4100%0301401
getNormal(FieldAbsoluteDate, Frame, FieldVector3D, FieldRotation)96100%4100%0301201
radiationPressureAcceleration(FieldAbsoluteDate, Frame, FieldVector3D, FieldRotation, RealFieldElement, FieldVector3D, RealFieldElement[])96100%8100%0501601
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[])85100%8100%0501601
getNormal(AbsoluteDate, Frame, Vector3D, Rotation)76100%4100%0301201
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, boolean, double, double)68100%2100%0201501
simpleBoxFacets(double, double, double)63100%n/a010101
facetRadiationAcceleration(FieldVector3D, double, FieldVector3D, RealFieldElement, RealFieldElement[])62100%n/a010701
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, boolean, double, double)58100%2100%0201501
facetRadiationAcceleration(Vector3D, double, Vector3D, double, double[])51100%n/a010701
filter(BoxAndSolarArraySpacecraft.Facet[])33100%4100%030501
getDragParametersDrivers()24100%2100%020101
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double)18100%n/a010201
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double, double)18100%n/a010201
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double)15100%n/a010201
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double)15100%n/a010201
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double, double)15100%n/a010201
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double, double)14100%n/a010201
getRadiationParametersDrivers()13100%n/a010101
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double)12100%n/a010201
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double, double)12100%n/a010201