diff --git a/Effects/model-wingflex.eff b/Effects/model-wingflex.eff
index dc609fb08..c6c3babb5 100644
--- a/Effects/model-wingflex.eff
+++ b/Effects/model-wingflex.eff
@@ -150,6 +150,14 @@
 		<wingsweep-factor>0.0</wingsweep-factor>
 		<wingflex-z>0.0</wingflex-z>
 		<wing-span>15.0</wing-span>
+		<!-- Sub: rotation -->
+		<rotation-rad type="float">0.0</rotation-rad>
+		<rotation-x1 type="float">0.0</rotation-x1>
+		<rotation-y1 type="float">0.0</rotation-y1>
+		<rotation-z1 type="float">0.0</rotation-z1>
+		<rotation-x2 type="float">0.0</rotation-x2>
+		<rotation-y2 type="float">0.0</rotation-y2>
+		<rotation-z2 type="float">0.0</rotation-z2>
 		<!-- END Wingflex -->
 		<cloudpos1_x><use>/local-weather/cloud-shadows/cloudpos-x[0]</use></cloudpos1_x>
 		<cloudpos1_y><use>/local-weather/cloud-shadows/cloudpos-y[0]</use></cloudpos1_y>
@@ -539,6 +547,48 @@
 				   <type>float</type>
 				   <value><use>wing-span</use></value>
 			   </uniform>
+
+		   	   <uniform>
+				   <name>rotation_rad</name>
+				   <type>float</type>
+				   <value><use>rotation-rad</use></value>
+			   </uniform>
+
+		   	   <uniform>
+				   <name>rotation_x1</name>
+				   <type>float</type>
+				   <value><use>rotation-x1</use></value>
+			   </uniform>
+
+		   	   <uniform>
+				   <name>rotation_y1</name>
+				   <type>float</type>
+				   <value><use>rotation-y1</use></value>
+			   </uniform>
+
+		   	   <uniform>
+				   <name>rotation_z1</name>
+				   <type>float</type>
+				   <value><use>rotation-z1</use></value>
+			   </uniform>
+			   
+		   	   <uniform>
+				   <name>rotation_x2</name>
+				   <type>float</type>
+				   <value><use>rotation-x2</use></value>
+			   </uniform>
+
+		   	   <uniform>
+				   <name>rotation_y2</name>
+				   <type>float</type>
+				   <value><use>rotation-y2</use></value>
+			   </uniform>
+
+		   	   <uniform>
+				   <name>rotation_z2</name>
+				   <type>float</type>
+				   <value><use>rotation-z2</use></value>
+			   </uniform>
 			   
 			   <!-- 			NORMAL MAP -->
 			   <!-- normalmap is used-->
diff --git a/Shaders/model-ALS-wingflex.vert b/Shaders/model-ALS-wingflex.vert
index b7e1d4d78..a8d06d94c 100644
--- a/Shaders/model-ALS-wingflex.vert
+++ b/Shaders/model-ALS-wingflex.vert
@@ -29,6 +29,13 @@ uniform float 		wingflex_trailing_alpha;
 uniform float 		wingsweep_factor;
 uniform float 		wingflex_z;
 uniform float		wing_span;
+uniform float		rotation_x1;
+uniform float		rotation_y1;
+uniform float		rotation_z1;
+uniform float		rotation_x2;
+uniform float		rotation_y2;
+uniform float		rotation_z2;
+uniform float		rotation_rad;
 uniform	int  		refl_dynamic;
 uniform int  		nmap_enabled;
 uniform int  		shader_qual;
@@ -55,6 +62,28 @@ void	rotationMatrixH(in float sinRz, in float cosRz, out mat4 rotmat)
 									0.0  ,	0.0  ,	0.0,	1.0 );
 }
 
+vec2 calc_deflection(float y){
+	float distance;
+	if(y < body_width && y > -body_width){
+		//this part does not move
+		distance = 0;
+	}else if(y > body_width){
+		distance = y - (body_width/2);
+	}else if(y < -body_width){
+		distance = y - ((-1*body_width)/2);
+	}
+	float max_dist = (wing_span-body_width)/2;
+	float deflection = wingflex_z * (distance*distance)/(max_dist*max_dist);
+	float delta_y;
+	if(y<0){
+		delta_y = deflection/wing_span;
+	}else{
+		delta_y = -deflection/wing_span;
+	}
+	vec2 returned = vec2 ( deflection, delta_y );
+	return returned;
+}
+
 void	main(void)
 {
 		vec4 vertex = gl_Vertex;
@@ -63,19 +92,49 @@ void	main(void)
 			float x_factor = max((abs(vertex.x) - body_width),0);
 			float y_factor = max(vertex.y,0.0);
 			
-			float distance;
-			if(vertex.y < body_width && vertex.y > -body_width){
-				//this part does not move
-				distance = 0;
-			}else if(vertex.y > body_width){
-				distance = vertex.y - (body_width/2);
-			}else if(vertex.y < -body_width){
-				distance = vertex.y - ((-1*body_width)/2);
-			}
-			float deflection = wingflex_z * (distance*distance)/(wing_span*wing_span);
+			vec2 deflection=calc_deflection(vertex.y);
+			
+			vertex.z += deflection[0];
+			vertex.y += deflection[1];
+			
+			if(rotation_rad != 0){
+				vec2 defl1=calc_deflection(rotation_y1);
+				vec2 defl2=calc_deflection(rotation_y2);
+				float rot_y1 = rotation_y1;
+				float rot_z1 = rotation_z1;
+				float rot_y2 = rotation_y2;
+				float rot_z2 = rotation_z2;
+				rot_y1 -= defl1[1];
+				rot_z1 += defl1[0];
+				rot_y2 -= defl2[1];
+				rot_z2 += defl2[0];
+				//Calculate rotation
+				vec3 normal;
+				normal[0]=rotation_x2-rotation_x1;
+				normal[1]=rot_y2-rot_y1;
+				normal[2]=rot_z2-rot_z1;
+				normal = normalize(normal);
+				float tmp = (1-cos(rotation_rad));
+				mat4 rotation_matrix = mat4(
+					pow(normal[0],2)*tmp+cos(rotation_rad),			normal[1]*normal[0]*tmp-normal[2]*sin(rotation_rad),	normal[2]*normal[0]*tmp+normal[1]*sin(rotation_rad),	0.0,
+					normal[0]*normal[1]*tmp+normal[2]*sin(rotation_rad),	pow(normal[1],2)*tmp+cos(rotation_rad),			normal[2]*normal[1]*tmp-normal[0]*sin(rotation_rad),	0.0,
+					normal[0]*normal[2]*tmp-normal[1]*sin(rotation_rad),	normal[1]*normal[2]*tmp+normal[0]*sin(rotation_rad),	pow(normal[2],2)*tmp+cos(rotation_rad),			0.0,
+					0.0,							0.0,							0.0,							1.0
+					);
+				vec4 old_point;
+				old_point[0]=vertex.x;
+				old_point[1]=vertex.y;
+				old_point[2]=vertex.z;
+				old_point[3]=1.0;
+				rotation_matrix[3][0] = rotation_x1 	- rotation_x1*rotation_matrix[0][0] - rot_y1*rotation_matrix[1][0] - rot_z1*rotation_matrix[2][0];
+				rotation_matrix[3][1] = rot_y1 	- rotation_x1*rotation_matrix[0][1] - rot_y1*rotation_matrix[1][1] - rot_z1*rotation_matrix[2][1];
+				rotation_matrix[3][2] = rot_z1 	- rotation_x1*rotation_matrix[0][2] - rot_y1*rotation_matrix[1][2] - rot_z1*rotation_matrix[2][2];
+				vec4 new_point=rotation_matrix*old_point;
+				vertex.x=new_point[0];
+				vertex.y=new_point[1];
+				vertex.z=new_point[2];
+			}
 			
-			vertex.z += deflection;
-			vertex.y -= deflection/wing_span;
 		} else if (wingflex_type == 1 ) {
 			float arm_reach = 4.8;
 
@@ -115,6 +174,8 @@ void	main(void)
 			if (vertex.x > 0.0) {sweep_x = - 0.5;}
 
 			vertex.x+= sweep_x * (1.0 + 0.5 *x_factor) *   wingsweep_factor;
+			
+			
 		}