GNSSAttitudeContext(AbsoluteDate, ExtendedPositionProvider, PVCoordinatesProvider, Frame, TurnSpan) | | 100% | | 100% | 0 | 3 | 0 | 21 | 0 | 1 |
turnCorrectedAttitude(UnivariateDerivative2) | | 100% | | n/a | 0 | 1 | 0 | 16 | 0 | 1 |
linearModelStillActive(double, double) | | 100% | | 100% | 0 | 3 | 0 | 12 | 0 | 1 |
lambda$linearModelStillActive$0(double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 13 | 0 | 1 |
setHalfSpan(double, double) | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
nominalYaw(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
orbitNormalYaw() | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
setUpTurnRegion(double, double) | | 100% | | 100% | 0 | 3 | 0 | 5 | 0 | 1 |
beta(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getYawEnd(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
static {...} | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getSecuredBeta() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
getYawStart(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getOrbitAngleSinceMidnight() | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
inTurnTimeRange() | | 100% | | 100% | 0 | 3 | 0 | 1 | 0 | 1 |
yawRate(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
inOrbitPlaneAbsoluteAngle(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
inSunSide() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
turnCorrectedAttitude(double, double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
computePhi(double, double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
timeSinceTurnStart() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
betaD2() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getTurnSpan() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getSVBcos() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDeltaDS() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMuRate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |