findRoot(OrekitStepInterpolator, AbsoluteDate, double, AbsoluteDate, double) | | 90% | | 85% | 11 | 38 | 3 | 83 | 0 | 1 |
check(boolean) | | 37% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
doEvent(SpacecraftState) | | 98% | | 80% | 2 | 6 | 0 | 14 | 0 | 1 |
tryAdvance(SpacecraftState, OrekitStepInterpolator) | | 98% | | 93% | 1 | 9 | 0 | 15 | 0 | 1 |
minTime(AbsoluteDate, AbsoluteDate) | | 93% | | 75% | 1 | 3 | 0 | 1 | 0 | 1 |
evaluateStep(OrekitStepInterpolator) | | 100% | | 92% | 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 |
shiftedBy(AbsoluteDate, double) | | 100% | | 100% | 0 | 4 | 0 | 9 | 0 | 1 |
lambda$findRoot$0(double, AbsoluteDate, AbsoluteDate, double, OrekitStepInterpolator, double) | | 100% | | 100% | 0 | 3 | 0 | 4 | 0 | 1 |
strictlyAfter(AbsoluteDate, AbsoluteDate) | | 100% | | 90% | 1 | 6 | 0 | 3 | 0 | 1 |
g(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 4 | 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 |