Started by GitHub push by lamont-granquist1513b25fedbbd80d7e43d663b788f5c447fd815599a8b25fedbbd80d7e43d663b788f5c447fd815599a8refs/remotes/origin/devb25fedbbd80d7e43d663b788f5c447fd815599a8b25fedbbd80d7e43d663b788f5c447fd815599a8refs/remotes/origin/devb25fedbbd80d7e43d663b788f5c447fd815599a8b25fedbbd80d7e43d663b788f5c447fd815599a8refs/remotes/origin/devhttps://github.com/MuMech/MechJeb2.gitMechJeb2-2.15.1.0-1513.zipMechJeb2-2.15.1.0-1513.zipMechJeb2-2.15.1.0-1513.zipfalse#15132068121569MechJeb2-Dev #15131513falsefalse15132384SUCCESS1767294579118https://ksp.sarbian.com/jenkins/user/videogamer0907/my-views/view/all/job/MechJeb2-Dev/1513/- MechJeb2/MechJebModuleAscentBaseAutopilot.csab7b6fc39490ec9a1d19831ccd9420dd9c3380791766763339000https://ksp.sarbian.com/jenkins/user/mailmailmail@diyar.chCommit fixes the bug from issue #2048
The bug occurs when using the autoascent feature for
negative inclination orbits. Namely, the circularization burn was
explicitly trying to achieve the _abs(inclination)_ instead of the target.
The bug was fixed by removing the `Math.Abs()` from the
OrbitalManeuverCalculator.DeltaVToChangeInclination input.
2025-12-26 16:35:39 +0100ab7b6fc39490ec9a1d19831ccd9420dd9c338079Commit fixes the bug from issue #2048editMechJeb2/MechJebModuleAscentBaseAutopilot.cs
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