Fix format

Author: 200km

src/dynamics/attitude/controlled_attitude.cpp

@@ -103,7 +103,9 @@ math::Vector<3> ControlledAttitude::CalcTargetDirection_i(AttitudeControlMode mo
     direction = OuterProduct(orbit_->GetPosition_i_m(), orbit_->GetVelocity_i_m_s());
   } else if (mode == AttitudeControlMode::kEarthSurfacePointing) {
     math::Vector<3> earth_surface_target_position_ecef_m = target_earth_surface_position_.CalcEcefPosition();
-    math::Vector<3> earth_surface_target_position_i_m = local_celestial_information_->GetGlobalInformation().GetEarthRotation().GetDcmJ2000ToEcef().Transpose()*earth_surface_target_position_ecef_m;
+    math::Vector<3> earth_surface_target_position_i_m =
+        local_celestial_information_->GetGlobalInformation().GetEarthRotation().GetDcmJ2000ToEcef().Transpose() *
+        earth_surface_target_position_ecef_m;
 
     direction = earth_surface_target_position_i_m - orbit_->GetPosition_i_m();
   }

src/dynamics/attitude/controlled_attitude.hpp

@@ -61,8 +61,8 @@ class ControlledAttitude : public Attitude {
   ControlledAttitude(const AttitudeControlMode main_mode, const AttitudeControlMode sub_mode, const math::Quaternion quaternion_i2b,
                      const math::Vector<3> main_target_direction_b, const math::Vector<3> sub_target_direction_b,
                      const math::Matrix<3, 3>& inertia_tensor_kgm2, const geodesy::GeodeticPosition target_earth_surface_position,
-                     const environment::LocalCelestialInformation* local_celestial_information,
-                     const orbit::Orbit* orbit, const std::string& simulation_object_name = "attitude");
+                     const environment::LocalCelestialInformation* local_celestial_information, const orbit::Orbit* orbit,
+                     const std::string& simulation_object_name = "attitude");
   /**
    * @fn ~ControlledAttitude
    * @brief Destructor
@@ -104,14 +104,14 @@ class ControlledAttitude : public Attitude {
   virtual void Propagate(const double end_time_s);
 
  private:
-  AttitudeControlMode main_mode_;             //!< Main control mode
-  AttitudeControlMode sub_mode_;              //!< Sub control mode
-  math::Vector<3> main_target_direction_b_;   //!< Main target direction on the body fixed frame
-  math::Vector<3> sub_target_direction_b_;    //!< Sub target direction on tge body fixed frame
-  double previous_calc_time_s_ = -1.0;        //!< Previous time of velocity calculation [sec]
-  math::Quaternion previous_quaternion_i2b_;  //!< Previous quaternion
-  math::Vector<3> previous_omega_b_rad_s_;    //!< Previous angular velocity [rad/s]
-  geodesy::GeodeticPosition target_earth_surface_position_; //!< Target position on the Earth surface
+  AttitudeControlMode main_mode_;                            //!< Main control mode
+  AttitudeControlMode sub_mode_;                             //!< Sub control mode
+  math::Vector<3> main_target_direction_b_;                  //!< Main target direction on the body fixed frame
+  math::Vector<3> sub_target_direction_b_;                   //!< Sub target direction on tge body fixed frame
+  double previous_calc_time_s_ = -1.0;                       //!< Previous time of velocity calculation [sec]
+  math::Quaternion previous_quaternion_i2b_;                 //!< Previous quaternion
+  math::Vector<3> previous_omega_b_rad_s_;                   //!< Previous angular velocity [rad/s]
+  geodesy::GeodeticPosition target_earth_surface_position_;  //!< Target position on the Earth surface
 
   const double kMinDirectionAngle_rad = 30.0 * math::deg_to_rad;  //!< Minimum angle b/w main and sub direction
                                                                   // TODO Change with ini file