Issues

Filters

Apply Clear

Toggle_check # Project Tracker Status Priority Subject Assignee Updated
370OrekitBugNewNormalWrong initialization of angular measurements' weights in W3B orbit determination tutorial and testMaxime Journot2017-11-16 11:22
369OrekitBugResolvedNormalError in the computation of the derivatives in Turn-Around Range ionospheric delay modifierMaxime Journot2017-11-08 12:01
367OrekitFeatureNewNormalAdd covariance to OEM writers2017-10-20 20:22
366OrekitBugNewNormalpotential (small) bug in SolarRadiationPressure2017-10-12 18:01
364OrekitBugResolvedNormalosculating to mean computation fails of eccentricity is exactly 02017-10-11 17:07
363OrekitBugResolvedNormalBug in DsstPropagator computeMeanState method2017-10-11 15:43
362OrekitBugResolvedNormalFiniteDifferencePropagatorConverter step size is scaled twiceEvan Ward2017-11-08 21:46
361OrekitBugResolvedNormalCCSDS OEMParser IAE for frame "ITRF2008"Evan Ward2017-11-08 21:46
360OrekitBugResolvedNormalCannot perform orbit estimation with both geopotential and solid tides force modelsLuc Maisonobe2017-09-07 14:08
359OrekitBugNewNormalIssues in orbit determination when selecting the central attraction coefficient as a parameter to estimateMaxime Journot2017-08-29 16:33
358OrekitFeatureNewNormalupdate the tolerance of a NumericalPropagator when change OrbitType2017-09-04 10:47
357OrekitBugResolvedLowminor error in code comments of DormandPrince853IntegratorBuilder2017-08-28 15:22
356OrekitBugResolvedLowearliest and latest dates unused in ShiftingTransformProvider and InterpolatingTransformProviderLuc Maisonobe2017-08-23 11:08
355OrekitBugResolvedNormalEarth inertial frame obtained from CelestialBodyFactory is wrongLuc Maisonobe2017-08-22 17:45
354OrekitBugResolvedNormalMapping of the propagation parameters for multi-satellite orbit determinationMaxime Journot2017-08-25 10:14
353OrekitFeatureResolvedNormalConvenience method to get standard covariance matrix from BatchLSEstimator2017-08-29 15:16
352OrekitBugResolvedNormalMistakes in the MariniMurrayMode class2017-08-28 12:27
351OrekitBugNewNormalPartialDerivativesEquations does not work with non-Cartesian elements2017-08-11 15:57
350OrekitBugResolvedNormalDifference in behavior between NumericalPropagator.addForceModel() and FieldNumericalPropagator().addForceModel()2017-08-28 11:57
349OrekitBugResolvedNormalImpulseManeuver does not forward additional states2017-08-28 11:01
343RuggedFeatureResolvedNormalAdd Danish error messages2017-06-21 13:41
256RuggedBugResolvedNormalSpacecraftToObservedBody: bad check of maxDate validityGuylaine Prat2016-10-18 12:50
242RuggedBugNewNormalInverseLocation: maybe inappropriate use of coarse threshold in SensorPixelCrossing2016-05-24 15:35
235Orekit python wrapperBugResolvedNormal'CelestialBody' does not have 'getPVCoordinates'2016-04-06 11:47
199OrekitBugNewLowimprove eclipse event handling in DSST Solar Radiation Pressure2015-04-30 19:26

1 2 (1-25/34) Per page: 25, 50

Also available in: Atom CSV PDF