findRoot(OrekitStepInterpolator, AbsoluteDate, double, AbsoluteDate, double) | | 94% | | 79% | 15 | 36 | 4 | 73 | 0 | 1 |
check(boolean) | | 38% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
minTime(AbsoluteDate, AbsoluteDate) | | 80% | | 50% | 2 | 3 | 0 | 1 | 0 | 1 |
shiftedBy(AbsoluteDate, double) | | 95% | | 83% | 1 | 4 | 1 | 9 | 0 | 1 |
doEvent(SpacecraftState) | | 99% | | 80% | 2 | 6 | 0 | 14 | 0 | 1 |
tryAdvance(SpacecraftState, OrekitStepInterpolator) | | 99% | | 93% | 1 | 8 | 0 | 11 | 0 | 1 |
evaluateStep(OrekitStepInterpolator) | | 100% | | 93% | 1 | 8 | 0 | 21 | 0 | 1 |
reinitializeBegin(OrekitStepInterpolator) | | 100% | | 100% | 0 | 5 | 0 | 15 | 0 | 1 |
EventState(EventDetector) | | 100% | | n/a | 0 | 1 | 0 | 15 | 0 | 1 |
strictlyAfter(AbsoluteDate, AbsoluteDate) | | 100% | | 90% | 1 | 6 | 0 | 3 | 0 | 1 |
g(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
lambda$findRoot$0(OrekitStepInterpolator, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
init(SpacecraftState, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
nextAfter(AbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getEventDetector() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEventDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |