NewtonianAttraction

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total21 of 10980%0 of 0n/a110320110
acceleration(SpacecraftState, double[])210%n/a113311
acceleration(FieldSpacecraftState, CalculusFieldElement[])27100%n/a010301
NewtonianAttraction(double)13100%n/a010301
getMu(Field, FieldAbsoluteDate)13100%n/a010201
addContribution(FieldSpacecraftState, FieldTimeDerivativesEquations)12100%n/a010301
addContribution(SpacecraftState, TimeDerivativesEquations)7100%n/a010201
getMu(AbsoluteDate)5100%n/a010101
static {...}5100%n/a010101
getParametersDrivers()4100%n/a010101
dependsOnPositionOnly()2100%n/a010101