BoxAndSolarArraySpacecraft

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total145 of 1,72191%10 of 7686%76826259030
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[], String)7716267%6857%48113601
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[], String)4410871%4866%3772601
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
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, boolean, double, double)75100%2100%0201601
getNormal(AbsoluteDate, Frame, Vector3D, Rotation)73100%4100%0301101
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, boolean, double, double)65100%2100%0201601
simpleBoxFacets(double, double, double)63100%n/a010101
facetRadiationAcceleration(FieldVector3D, double, FieldVector3D, RealFieldElement, RealFieldElement[])62100%n/a010701
facetRadiationAcceleration(Vector3D, double, Vector3D, double, double[])51100%n/a010701
facetRadiationAcceleration(Vector3D, double, Vector3D, double, DerivativeStructure, DerivativeStructure)37100%n/a010501
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