diff --git a/AirLib/include/common/VectorMath.hpp b/AirLib/include/common/VectorMath.hpp
index 391a668b0d..7eaeb1a9e6 100644
--- a/AirLib/include/common/VectorMath.hpp
+++ b/AirLib/include/common/VectorMath.hpp
@@ -207,19 +207,20 @@ class VectorMathT {
     static void toEulerianAngle(const QuaternionT& q
         , RealT& pitch, RealT& roll, RealT& yaw)
     {
+        // https://en.wikipedia.org/wiki/Conversion_between_quaternions_and_Euler_angles
         RealT ysqr = q.y() * q.y();
         RealT t0 = -2.0f * (ysqr + q.z() * q.z()) + 1.0f;
         RealT t1 = +2.0f * (q.x() * q.y() + q.w() * q.z());
-        RealT t2 = -2.0f * (q.x() * q.z() - q.w() * q.y());
-        RealT t3 = +2.0f * (q.y() * q.z() + q.w() * q.x());
-        RealT t4 = -2.0f * (q.x() * q.x() + ysqr) + 1.0f;
+        roll = std::atan2(t1, t0);
 
+        RealT t2 = -2.0f * (q.x() * q.z() - q.w() * q.y());
         t2 = t2 > 1.0f ? 1.0f : t2;
         t2 = t2 < -1.0f ? -1.0f : t2;
-
         pitch = std::asin(t2);
-        roll = std::atan2(t3, t4);
-        yaw = std::atan2(t1, t0);
+
+        RealT t3 = +2.0f * (q.y() * q.z() + q.w() * q.x());
+        RealT t4 = -2.0f * (q.x() * q.x() + ysqr) + 1.0f;
+        yaw = std::atan2(t3, t4);
     }
 
     static Vector3T toAngularVelocity(const QuaternionT& start, const QuaternionT& end, RealT delta_sec)