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Fixes negative inclination circularization from Autoascent #2054

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Fixes negative inclination circularization from Autoascent #2054

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2 changes: 1 addition & 1 deletion MechJeb2/MechJebModuleAscentBaseAutopilot.cs
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Original file line number Diff line number Diff line change
Expand Up @@ -267,7 +267,7 @@ private void DriveCircularizationBurn()
// FIXME? this inclination correction is unlikely to be at tha AN/DN and will throw the LAN off with anything other than high
// TWR launches from equatorial launch sites -- should probably be made optional (or clip it if the correction is too large).
Vector3d inclinationCorrection =
OrbitalManeuverCalculator.DeltaVToChangeInclination(Orbit, ut, Math.Abs(AscentSettings.DesiredInclination));
OrbitalManeuverCalculator.DeltaVToChangeInclination(Orbit, ut, AscentSettings.DesiredInclination);
Vector3d smaCorrection = OrbitalManeuverCalculator.DeltaVForSemiMajorAxis(Orbit.PerturbedOrbit(ut, inclinationCorrection), ut,
AscentSettings.DesiredOrbitAltitude + MainBody.Radius);
Vector3d dV = inclinationCorrection + smaCorrection;
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