diff --git a/ovm/task2.c b/ovm/task2.c
index 194b6e5..37c8f93 100644
--- a/ovm/task2.c
+++ b/ovm/task2.c
@@ -100,7 +100,6 @@ static void run(task_t *task, gpointer userdata) {
 			start_hohmann = starttime ;
 			if (sat.move.v.x * S_Y > 0.0 && sat.move.v.y * S_X < 0.0) target_v = -target_v;
 			printf("Vorsprung für Target: %u (Winkel: %14.3f)\n", start_hohmann, (180.0*phi/M_PI));
-// 			printf("T: %14.3f\n", 2*M_PI*target_sat.rad*sqrt(target_sat.rad/(G*Me)));
 		} else if (start_hohmann == task->timestamp) {
 			satellite_update_move(&sat);
 			DV_X = sat.move.v.x * (dv / sat.move.v_abs);
@@ -122,49 +121,13 @@ static void run(task_t *task, gpointer userdata) {
 				printf("Dv: %f / %f\n", DV_X, DV_Y);
 			}
 		}
-#if 0
-	} else if (DISTANCE > 400) {
-		gdouble dx = task->out[4], dy = task->out[5];
-#endif
-#if 0
-	} else if (DISTANCE > 500.0) {
-		gdouble phidiff = 180.0*(atan2(S_Y, S_X) - atan2(T_Y, T_X))/M_PI;
-		gdouble target_rad = target_sat.rad - sat.rad;
-/*		gdouble tar_dv_x = -target_v * S_Y / sat.rad;
-		gdouble tar_dv_y = target_v * S_X / sat.rad;*/
-		satellite_update_move(&sat);
-		printf("Distance: %14.3f\n", phidiff);
-		if (phidiff < 0 || phidiff > 180.0) { /* slow down */
-			target_rad += 20.0;
-		} else { /* speed up */
-			target_rad -= 20.0;
-		}
-		target_rad = fmax(-5.0, fmin(5.0, target_rad));
-		DV_X = /*tar_dv_x - sat.move.v.x*/ + target_rad * S_X / sat.rad;
-		DV_Y = /*tar_dv_y - sat.move.v.y*/ + target_rad * S_Y / sat.rad;
-			printf("v: %f / %f\n", sat.move.v.x, sat.move.v.y);
-			printf("Dv: %f / %f\n", DV_X, DV_Y);
-		debug(task);
-#endif
 	} else if (!outoffuel) {
+		/* target_v is clockwise */
+		gdouble tar_dv_x = -target_v * S_Y / sat.rad;
+		gdouble tar_dv_y = target_v * S_X / sat.rad;
 		satellite_update_move(&sat);
-		if (FALSE && fabs(sat.rad - target_sat.rad) > 3) {
-			gdouble tar_dv_x = -target_v * S_Y / sat.rad;
-			gdouble tar_dv_y = target_v * S_X / sat.rad;
-			gdouble target_rad = target_sat.rad - sat.rad;
-			target_rad = fmax(-10.0, fmin(10.0, target_rad));
-			DV_X = tar_dv_x - sat.move.v.x + target_rad * S_X / sat.rad;
-			DV_Y = tar_dv_y - sat.move.v.y + target_rad * S_Y / sat.rad;
-			printf("-- orbit correction\n");
-			printf("v: %f / %f\n", sat.move.v.x, sat.move.v.y);
-			printf("Dv: %f / %f\n", DV_X, DV_Y);
-		} else {
-			/* target_v is clockwise */
-			gdouble tar_dv_x = -target_v * S_Y / sat.rad;
-			gdouble tar_dv_y = target_v * S_X / sat.rad;
-			DV_X = tar_dv_x - sat.move.v.x;
-			DV_Y = tar_dv_y - sat.move.v.y;
-		}
+		DV_X = tar_dv_x - sat.move.v.x;
+		DV_Y = tar_dv_y - sat.move.v.y;
 		if (DV_X*DV_X + DV_Y*DV_Y > FUEL*FUEL) {
 			printf("-- Out of fuel\n");
 			printf("v: %f / %f\n", sat.move.v.x, sat.move.v.y);