Merge branch 'feature/github_action' of https://github.com/valeriof7/…

…tudat into feature/github_action

include/tudat/astro/aerodynamics/aerodynamicAcceleration.h

@@ -38,7 +38,7 @@ namespace aerodynamics
  * \return Resultant aerodynamic acceleration, given in reference frame in which the
  *          aerodynamic coefficients were given (assuming coefficients in positive direction).
  */
-Eigen::Vector3d computeAerodynamicAcceleration(      const double dynamicPressure,
+Eigen::Vector3d computeAerodynamicAcceleration( const double dynamicPressure,
                                                 const double referenceArea,
                                                 const Eigen::Vector3d& aerodynamicCoefficients,
                                                 const double vehicleMass );