VERSION 1.0

INFO	                  //Free Form Comment Area, does not change model
Name: GWS Formosa         //Plane Name
Aerobatic ParkFlyer       //Type of Plane
Spannweite: 0.91 m        //Span (m)
Gewicht:     .41 kg       //Weight (kg)
Motorisierung: EPS-350C   //Engine
Prop: 9x7, 10x6           //Prop
Akku: 7 cell	          //Battery (6 Zellen = 6 cells)
Kapazit鋞 des Akkus: 750mAh //Battery Capacity
	
RC-Funktionen:            //RC Functions
Kanal 1: Rudder           //Channel 1 (Seitenruder = rudder, Heckrad = tail wheel)
Kanal 2: Elevator         //Channel 2 (H鰄enruder = elevator)
Kanal 3: Aileron          //Channel 3 (Querruder = Aileron) 
Kanal 4: Motor            //Channel 4 (Motordrossel = Engine Throttle)
	
Author: Gary Gunnerson http://gunnerson.homestead.com/files/fms_models.htm GaryG51384@aol.com

ENDINFO	                  //ENDINFO, end comment area

// <ParEditor Ver0.6 2005-04-01 Masuoka Hideaki>
// ParEditor.Scale=164
// ParEditor.Data1=	2	2	1	1.0000	3	3.0822	7.2221
// ParEditor.Data2=0.5	0.2576	0.2576	0.0672	0.0384	0.4224	0.8	2.3432
// ParEditor.Data3=0	0	0
// ParEditor.Data4=0	0	2	2	-1	-5				
// ParEditor.Data5=2	-2	1	-1	0	0				
// ParEditor.Data6=1	1	0	0	-2	1				
// ParEditor.Data7=15	8.628

AIRPLANE

MAIN

1.0                           //Mass [Kg]
0.0432                        //Roll Inertia Moment Ixx [kg*m^2]
0.1127                        //Pitch Inertia Moment Iyy [kg*m^2]
0.1758                        //Yaw Inertia Moment Izz [kg*m^2]
0                             //Ixz [kg*m^2]
0.06 0 0                      //廳怱埵抲X,Y,Z [m]
0.33                          //Height of Center of gravity [m]

MOTOR

//MOTOR1
0.37 0 -0.014                 //僾儘儁儔埵抲 [m]
1 0 0                         //悇椡儀僋僩儖 X,Y,Z
0.30                          //propeller diameter [m]
.2                            //pitch, upward gradient of propeller [m]
2                             //number of propeller blades
0.015                         //mean chord length of propeller blades [m]
RIGHT                         //Rotation(RIGHT/LEFT)
0.0002                        //moment of inertia [kg*m^2]
4                             //channel
ELECTRO                       //COMBUSTION/ELECTRO
9.6                           //motor voltage [V]
18000                         //idling speed [rpm]
1                             //idling current [A]
85                            //blocking current [A]
1                             //Gear ratio
1                             //Gear efficiency
8                             //number of batt cells
1150                          //capacity of batts [mAh]
5                             //internal battery resistance [mohm]

WING

//WING1 <LWING>
0.09 -0.28 0.01               //梼埵抲X,Y,Z [m]
0.9976 -0.0697 -0.0037        //Ex X,Y,Z
0.0698 0.9962 0.0522          //Ey X,Y,Z
1                             //polar number
0.56                          //span [m]
4                             //number of elements
AUTOELEMENT
1                             //Angle [deg]
0.18                          //chord length at the first end [m]
0.28                          //chord length at the second end [m]
0.06                          //chord length of the flap [m]
0                             //start position of the flap [m]
0.56                          //end position of the flap [m]
-20                           //Maximum Angle [deg]
3                             //channel

//WING2 <RWING>
0.09 0.28 0.01                //梼埵抲X,Y,Z [m]
0.9976 0.0697 -0.0037         //Ex X,Y,Z
-0.0698 0.9962 -0.0522        //Ey X,Y,Z
1                             //polar number
0.56                          //span [m]
4                             //number of elements
AUTOELEMENT
1                             //Angle [deg]
0.28                          //chord length at the first end [m]
0.18                          //chord length at the second end [m]
0.06                          //chord length of the flap [m]
0                             //start position of the flap [m]
0.56                          //end position of the flap [m]
20                            //Maximum Angle [deg]
3                             //channel

//WING3 <ELEVATOR>
-0.54 0 0.01                  //梼埵抲X,Y,Z [m]
1 0 0                         //Ex X,Y,Z
0 1 0                         //Ey X,Y,Z
2                             //polar number
0.48                          //span [m]
4                             //number of elements
AUTOELEMENT
-1                            //Angle [deg]
0.14                          //chord length at the first end [m]
0.14                          //chord length at the second end [m]
0.04                          //chord length of the flap [m]
0                             //start position of the flap [m]
0.48                          //end position of the flap [m]
20                            //Maximum Angle [deg]
2                             //channel

//WING4 <RUDDER>
-0.54 0 -0.038                //梼埵抲X,Y,Z [m]
1 0 0                         //Ex X,Y,Z
0 0 -1                        //Ey X,Y,Z
2                             //polar number
0.24                          //span [m]
4                             //number of elements
AUTOELEMENT
0                             //Angle [deg]
0.18                          //chord length at the first end [m]
0.14                          //chord length at the second end [m]
0.10                          //chord length of the flap [m]
0                             //start position of the flap [m]
0.24                          //end position of the flap [m]
-24                           //Maximum Angle [deg]
1                             //channel

//WING5 <BODY>
0.16 0 -0.02                  //梼埵抲X,Y,Z [m]
1 0 0                         //Ex X,Y,Z
0 0 -1                        //Ey X,Y,Z
3                             //polar number
0.16                          //span [m]
3                             //number of elements
AUTOELEMENT
0                             //Angle [deg]
0.88                          //chord length at the first end [m]
0.88                          //chord length at the second end [m]
0                             //chord length of the flap [m]
0                             //start position of the flap [m]
0                             //end position of the flap [m]
0                             //Maximum Angle [deg]
0                             //channel

DRAG

0.0053 0 -0.0064              //掞峈埵抲X,Y,Z [m]
0.005                         //reference cross section [m^2]
0.1                           //Drag Coefficient
0                             //channel

POLAR

//POLAR1
18                            //僨乕僞悢
-180 0 0.03 0                 //寎妏(deg),CL,CD,CM
-170 0.63 0.1 0
-90 0 1.2 0.3
-50 -1.1 0.96 0.21
-21 -0.77 0.48 0.1
-14 -0.72 0.25 0.08
-13 -0.92 0.07 0
-9 -0.84 0.045 0
-3.5 -0.35 0.025 0
3.5 0.35 0.025 0
9 0.84 0.045 0
13 0.92 0.07 0
14 0.72 0.25 -0.08
21 0.77 0.48 -0.1
50 1.1 0.96 -0.21
90 0 1.2 -0.3
170 -0.63 0.1 0
180 0 0.03 0
-12                           //angle of attack lower flow separation [deg]
12                            //angle of attack upper flow separation [deg]
1.5                           //flow separation hysteresis [deg]

//POLAR2
18                            //僨乕僞悢
-180 0 0.03 0                 //寎妏(deg),CL,CD,CM
-170 0.63 0.1 0
-90 0 1.2 0.3
-50 -0.9 1 0.21
-20 -0.6 0.58 0.12
-10.5 -0.57 0.28 0.1
-10 -0.71 0.07 0
-8.2 -0.67 0.045 0
-2.5 -0.28 0.025 0
2.5 0.28 0.025 0
8.2 0.67 0.045 0
10 0.71 0.07 0
10.5 0.57 0.28 -0.1
20 0.6 0.58 -0.12
50 0.9 1 -0.21
90 0 1.2 -0.3
170 -0.63 0.1 0
180 0 0.03 0
-10                           //angle of attack lower flow separation [deg]
10                            //angle of attack upper flow separation [deg]
1                             //flow separation hysteresis [deg]

//POLAR3
17                            //僨乕僞悢
-180 0 0.03 0                 //寎妏(deg),CL,CD,CM
-170 0.4 0.1 0
-90 0 1.2 0.3
-50 -0.7 0.96 0.21
-30 -0.55 0.63 0.16
-13 -0.25 0.19 0.13
-9.01 -0.14 0.07 0.1
-9 -0.45 0.04 0.07
0 0 0.032 0
9 0.45 0.04 -0.07
9.01 0.14 0.07 -0.1
13 0.25 0.19 -0.13
30 0.55 0.63 -0.16
50 0.7 0.96 -0.21
90 0 1.2 -0.3
170 -0.4 0.1 0
180 0 0.03 0
-9                            //angle of attack lower flow separation [deg]
9                             //angle of attack upper flow separation [deg]
2                             //flow separation hysteresis [deg]

POINT                         //3D嫬奅埵抲

//POINT1
-0.11767 0.94119 0.01621      //億僀儞僩埵抲 [m]
1200                          //spring constant [N/m]
35                            //Viscosity [N*s/m]
50                            //breaking load [N]
1.2                           //coefficent of friction

//POINT2
-0.11767 -0.94119 0.01621     //億僀儞僩埵抲 [m]
1200                          //spring constant [N/m]
35                            //Viscosity [N*s/m]
80                            //breaking load [N]
1.2                           //coefficent of friction

//POINT3
0.62198 0 -0.27027            //億僀儞僩埵抲 [m]
1200                          //spring constant [N/m]
35                            //Viscosity [N*s/m]
80                            //breaking load [N]
1.2                           //coefficent of friction

//POINT4
0.62198 0 0.22156             //億僀儞僩埵抲 [m]
1200                          //spring constant [N/m]
35                            //Viscosity [N*s/m]
80                            //breaking load [N]
1.2                           //coefficent of friction

//POINT5
-1.097 0 0.08714              //億僀儞僩埵抲 [m]
1200                          //spring constant [N/m]
35                            //Viscosity [N*s/m]
80                            //breaking load [N]
1.2                           //coefficent of friction

//POINT6
-1.095 0 -0.23026             //億僀儞僩埵抲 [m]
1200                          //spring constant [N/m]
35                            //Viscosity [N*s/m]
80                            //breaking load [N]
1.2                           //coefficent of friction

WHEEL                         //幵椫

//WHEEL1
0.30121 -0.31917 .34          //幵椫埵抲 [m]
1000                          //spring constant [N/m]
20                            //Viscosity [N*s/m]
100                           //breaking load [N]
0 -1 0                        //幵幉儀僋僩儖 [X,Y,Z]
0.18                          //coefficient of friction trace direction
0.7                           //coeff. of fric. transverse direction
0                             //channel
0                             //Maximum Angle [deg]

//WHEEL2
0.30121 0.31917 .34           //幵椫埵抲 [m]
1000                          //spring constant [N/m]
20                            //Viscosity [N*s/m]
100                           //breaking load [N]
0 1 0                         //幵幉儀僋僩儖 [X,Y,Z]
0.18                          //coefficient of friction trace direction
0.7                           //coeff. of fric. transverse direction
0                             //channel
0                             //Maximum Angle [deg]

//WHEEL3
-1.026 0 .19                  //幵椫埵抲 [m]
1200                          //spring constant [N/m]
20                            //Viscosity [N*s/m]
100                           //breaking load [N]
0 1 0                         //幵幉儀僋僩儖 [X,Y,Z]
0.18                          //coefficient of friction trace direction
0.7                           //coeff. of fric. transverse direction
1                             //channel
-20                           //Maximum Angle [deg]

