Started by GitHub push by lamont-granquistStarted by GitHub push by lamont-granquist1644fc9a56a90f3eb42d8856745efa777a2dfc70ff20fc9a56a90f3eb42d8856745efa777a2dfc70ff20refs/remotes/origin/devfc9a56a90f3eb42d8856745efa777a2dfc70ff20fc9a56a90f3eb42d8856745efa777a2dfc70ff20refs/remotes/origin/devfc9a56a90f3eb42d8856745efa777a2dfc70ff20fc9a56a90f3eb42d8856745efa777a2dfc70ff20refs/remotes/origin/devhttps://github.com/MuMech/MechJeb2.githttps://ksp.sarbian.com/jenkins/user/andy/my-views/view/All/job/MechJeb2-Dev/1644/artifacthttps://ksp.sarbian.com/jenkins/user/andy/my-views/view/All/job/MechJeb2-Dev/changeshttps://ksp.sarbian.com/jenkins/user/andy/my-views/view/All/job/MechJeb2-Dev/1644/https://ksp.sarbian.com/jenkins/user/andy/my-views/view/All/job/MechJeb2-Dev/1644/testReportMechJeb2-2.16.0.0-1644.zipMechJeb2-2.16.0.0-1644.zipMechJeb2-2.16.0.0-1644.zipfalse#16442926928533MechJeb2-Dev #16441644falsefalse164469SUCCESS1780374818435https://ksp.sarbian.com/jenkins/user/andy/my-views/view/All/job/MechJeb2-Dev/1644/- MechJebLib/Maneuvers/ChangeOrbitalElement.csMechJebLibTest/ManeuversTests/ChangeOrbitalElementTests.cs7c9dc025201d9465d249a8870f2a27b63a876b931780374619000https://ksp.sarbian.com/jenkins/user/lamontlamontlamont@scriptkiddie.orgConvert ChangeOrbitalElements to use AUL+SQP
Turns out the landscape through parabolic orbits for the ecc problem
really is C0-smooth, but the SQP solver still gets caught up on the
transition. So presolve with AUL first, then sharpen with SQP, then
the special initialization for the ecc problem can be dropped.
2026-06-01 21:30:19 -07007c9dc025201d9465d249a8870f2a27b63a876b93Convert ChangeOrbitalElements to use AUL+SQPeditMechJebLibTest/ManeuversTests/ChangeOrbitalElementTests.cseditMechJebLib/Maneuvers/ChangeOrbitalElement.cs
githttps://ksp.sarbian.com/jenkins/user/lamontlamontlamont