StateTransitionMatrixGenerator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total2 of 72999%1 of 3296%126191010
setInitialStateTransitionMatrix(SpacecraftState, RealMatrix, OrbitType, PositionAngle)10398%11191%1712001
computePartials(SpacecraftState)329100%16100%0904701
multiplyMatrix(double[], double[], double[], int)234100%2100%020701
derivatives(SpacecraftState)20100%n/a010501
StateTransitionMatrixGenerator(String, List, AttitudeProvider)17100%n/a010601
yield(SpacecraftState)9100%2100%020101
addObserver(String, StateTransitionMatrixGenerator.PartialsObserver)7100%n/a010201
getName()3100%n/a010101
static {...}3100%n/a010101
getDimension()100%n/a010101