fix: state frame conversion in ComputeTargetDirectionVector (#438)

open-space-collective · Sep 20, 2024 · af0155d · af0155d
1 parent 19b96f5
commit af0155d
Showing 1 changed file with 1 addition and 1 deletion.
diff --git a/src/OpenSpaceToolkit/Astrodynamics/Flight/Profile.cpp b/src/OpenSpaceToolkit/Astrodynamics/Flight/Profile.cpp
@@ -407,7 +407,7 @@ Vector3d Profile::ComputeTargetDirectionVector(const State& aState, const Trajec
     }
 
     const Vector3d targetPositionCoordinates =
-        aTrajectory.getStateAt(aState.accessInstant()).getPosition().accessCoordinates();
+        aTrajectory.getStateAt(aState.accessInstant()).inFrame(Frame::GCRF()).getPosition().accessCoordinates();
     const Vector3d satellitePositionCoordinates = aState.getPosition().accessCoordinates();
 
     return (targetPositionCoordinates - satellitePositionCoordinates).normalized();