diff --git a/src/modules/fw_dyn_soar_control/FixedwingPositionINDIControl.cpp b/src/modules/fw_dyn_soar_control/FixedwingPositionINDIControl.cpp
index d22d9a1ece..b1977521d0 100644
--- a/src/modules/fw_dyn_soar_control/FixedwingPositionINDIControl.cpp
+++ b/src/modules/fw_dyn_soar_control/FixedwingPositionINDIControl.cpp
@@ -440,13 +440,13 @@ FixedwingPositionINDIControl::soaring_estimator_shear_poll()
 			// the initial speed of the target trajectory can safely be updated during soaring :)
 			_shear_aspd = _soaring_estimator_shear.aspd;
 			_param_shear_estimated_v_max.set(_shear_v_max);
-			_param_shear_estimated_v_max.commit()
+			_param_shear_estimated_v_max.commit();
 			_param_shear_estimated_alpha.set(_shear_alpha);
-			_param_shear_estimated_alpha.commit()
+			_param_shear_estimated_alpha.commit();
 			_param_shear_estimated_h_ref.set(_shear_h_ref);
-			_param_shear_estimated_h_ref.commit()
+			_param_shear_estimated_h_ref.commit();
 			_param_shear_estimated_heading.set(_shear_heading);
-			_param_shear_estimated_heading.commit()
+			_param_shear_estimated_heading.commit();
 		}
 
 	}
@@ -697,8 +697,8 @@ FixedwingPositionINDIControl::_read_trajectory_coeffs_csv(char *filename)
 	// =======================================================================
 	bool error = false;
 
-	//char home_dir[200] = "/home/marvin/Documents/master_thesis_ADS/PX4/Git/ethzasl_fw_px4/src/modules/fw_dyn_soar_control/trajectories/";
-	char home_dir[200] = PX4_ROOTFSDIR"/fs/microsd/trajectories/";
+	char home_dir[200] = "/home/jaeyoung/src/PX4-Autopilot/src/modules/fw_dyn_soar_control/trajectories/";
+	// char home_dir[200] = PX4_ROOTFSDIR"/fs/microsd/trajectories/";
 	//PX4_ERR(home_dir);
 	strcat(home_dir, filename);
 	FILE *fp = fopen(home_dir, "r");
diff --git a/src/modules/fw_dyn_soar_control/fw_dyn_soar_control_params.c b/src/modules/fw_dyn_soar_control/fw_dyn_soar_control_params.c
index 21eec6fcb8..897e61c615 100644
--- a/src/modules/fw_dyn_soar_control/fw_dyn_soar_control_params.c
+++ b/src/modules/fw_dyn_soar_control/fw_dyn_soar_control_params.c
@@ -475,7 +475,7 @@ PARAM_DEFINE_FLOAT(DS_K_DAMP_PITCH, 0.02f);
  * @increment 0.0000001
  * @group FW DYN SOAR Control
  */
-PARAM_DEFINE_FLOAT(DS_ORIGIN_LAT, 47.3130000f);
+PARAM_DEFINE_FLOAT(DS_ORIGIN_LAT, 47.397754f);
 
 /**
  * longitude of trajectory start point (WGS84)
@@ -487,7 +487,7 @@ PARAM_DEFINE_FLOAT(DS_ORIGIN_LAT, 47.3130000f);
  * @increment 0.0000001
  * @group FW DYN SOAR Control
  */
-PARAM_DEFINE_FLOAT(DS_ORIGIN_LON, 8.8100000f);
+PARAM_DEFINE_FLOAT(DS_ORIGIN_LON, 8.546372f);
 
 /**
  * altitude of trajectory start point (WGS84)