// AI Helicopter configuration files
// by Holger Sandmann (hsandman@sfu.ca) 
// and Doug Callihan
// 
// Version 1, May 2003
//
// for Aerospatiale/Eurocopter AS365N3 Dauphin GMax
// by Antti Pankkonen, apankkon@cc.hut.fi
//
// based on Stemme motor glider aircraft.cfg
// by Al Kaiser, kaiser@va-works.com or http://www.va-works.com/
//
// !!!Copyright remains with the original authors!!!


[Fltsim.0]
Title=MHAI AS32 HAF
Sim=stemme_as_helicopter_2
Model=
Panel=
Sound=
Texture=HAF
Prop_anim_ratio=-1.76
Atc_id_color=0xc6eff7ff
Atc_id=
Atc_model=AS-332C1
Ui_manufacturer=Aerospatiale
Ui_type=AS-332C1 Super Puma
Ui_variation=Hellenic Air Force SAR 358th Sqdr
Atc_flight_number=
Atc_heavy=0
Atc_airline=Hellenic Air Force
Visual_damage=1
Description=Hellenic Air Force 358 Sqdr ''Search And Rescue'' repaint created by Nick Karatzides (e-mail: Nick_Karatzides@hotmail.com OR pathfinder@mail.gr) as an honor to the 358th Sqdr of Hellenic Air Force based in Elefsina, Greece with a SAR (Search And Rescue) role. Original model & repaint by Dirk Fassbender (e-mail: email@dirkfassbender.de) (site: www.dirkfassbender.de).
atc_parking_codes=AS32,M004
atc_parking_types=RAMP

[General]
atc_type=Aerospatiale
atc_model=AS365
performance=Cruise Speed	149 kts @ 3750 kg\nMaximum Range	483 nm @ 3750 kg\nService Ceiling	>15 000 ft\nHovering Ceiling	10 203 ft, O.G.E.\nMax Gross Weight   4300 kg\nHook Load Limit 	1600  kg\nSeating		1-2 pilots + 11 passengers\nUseful Load	1944 kg

//---- misc tweaked parameters 

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position= 0.000,0.000,-2.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000

max_gross_weight=2300	// (pounds)
empty_weight=1300

;Moments of Inertia
empty_weight_pitch_MOI=3000
empty_weight_roll_MOI=4000
empty_weight_yaw_MOI=9000
empty_weight_coupled_MOI=-1000

CG_forward_limit=0.000
CG_aft_limit=1.000

[Reference Speeds]
flaps_up_stall_speed=30
full_flaps_stall_speed=27
cruise_speed=115
max_indicated_speed=180.000000

[flight_tuning]
cruise_lift_scalar=1.25 		// was 1.15
parasite_drag_scalar=0.8 		// was 0.8
induced_drag_scalar=0.8 		// was 0.8
elevator_effectiveness=1.5 		// was 1.0
aileron_effectiveness=1.0 
rudder_effectiveness=2.0   		// was 1.5
pitch_stability=1.0 
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.9	 	// was 1.0

[flaps.0]       		//Trailing Edge Flaps
type=1          		// 1 - tail, 2 - lead
span-outboard=0.600   	// 0.0 .. 1.0
extending-time=4.000  	// seconds
flaps-position.0=0    	// degrees
flaps-position.1=0   	// degrees           
flaps-position.2=20  	// degrees           
flaps-position.3=30	// degrees
damaging-speed=200   	// KIAS       
blowout-speed=250    	// KIAS
lift_scalar=1.3	 
drag_scalar=0.8
pitch_scalar=1.2
system_type=0        	//0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None



//---- parameters from AS365 Dauphin, tweaked

//0  Class                        <0=none,1=wheel, 2=scrape, 3=skid>
//1  Longitudinal Position        (feet)
//2  Lateral Position             (feet)
//3  Vertical Position            (feet)
//4  Impact Damage Threshold      (Feet Per Minute)
//5  Brake Map                    (0=None, 1=Left, 2=Right)
//6  Wheel Radius                 (feet)
//7  Steer Angle                  (degrees)
//8  Static Compression           (feet)  (0 if rigid)
//9  Max/Static Compression Ratio
//10 Damping Ratio                (0=Undamped, 1=Critically Damped)
//11 Extension Time               (seconds)
//12 Retraction Time              (seconds)
//13 Sound Type
//14 Airspeed limit for retraction     (KIAS)
//15 Airspeed that gear gets damage at (KIAS)

[Contact_Points]
Point.0=1, 10.8246, 0, -0.6246, 1500, 0, 1, 90, 0.3, 2.5, 0.5, 0.01, 0.01, 0, 200, 200
Point.1=1, -6.3273, -5.3, -0.8737, 1500, 1, 1, 0, 0.3, 2.5, 0.5, 0.01, 0.01, 2, 200, 200
Point.2=1, -6.5765, 5.3, -0.8737, 1500, 2, 1, 0, 0.3, 2.5, 0.5, 0.01, 0.01, 3, 200, 200
Point.3=2, 14.6285, -4, 1.4491, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
Point.4=2, 14.753, 4, 1.4489, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
Point.5=2, -0.1584, -22.4556, 12.6625, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
Point.6=2, -0.0341, 22.4563, 12.9118, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
Point.7=2, -33.875, 0, 3.1227, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0
Static_pitch=0
Static_cg_height=0.63
Max_number_of_points=8
gear_system_type=3

[Views]
eyepoint=-0.72,1.4,3.2

[Lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
Light.0=3, -5.48, -5.98, 3.48, fx_navred
Light.1=4, -6.34, -0.10, 8.08, fx_navwhi
Light.2=4, 5.05, 0.00, 8.14, fx_navwhi
Light.3=3, -5.46, 6.08, 3.35, fx_navgre
//Light.4=3, -34.26,  0.00, 11.88,  fx_navwhi ,
//Light.5=3, -36.3, 0, 10.69, fx_navwhi
Light.6=1, -34.75,  0.00, 11.93,  fx_beacon ,
Light.7=4, 12.31, -1.74, 6.62, fx_navgre
Light.8=4, -10.28, -0.24, 7.76, fx_navwhi
Light.9=4, 12.33, 1.66, 6.6, fx_navgre
Light.10=4, 0.12, 0, 7.97, fx_navwhi

[effects]
water=fx_spray
dirt = fx_tchdrt
concrete = fx_tchdrt, 1
touchdown = fx_dustcloud_m, 1
startup=fx_engstrt

//touchdown = fx_tchdwn, 1
//landrotorwash = fx_rtr_lnd
//waterrotorwash = fx_rtr_wtr



//---- parameters from Stemme motor glider, tweaked

[fuel]
LeftMain=-0.250000,-2.100000,2.500000,6.000000,0.000000
RightMain=-0.250000,2.100000,2.500000,6.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=1

[airplane_geometry]
wing_area=400				// was 201.0
wing_span=60				// was 57.0
wing_root_chord=4.916670
wing_dihedral=3.499146
wing_incidence=4.999268 		// was 2.999268
wing_twist=-1.994019
oswald_efficiency_factor=.448140	// was 1.064814  
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=1.229000
wing_pos_apex_vert=0.000000
htail_area=16.000000
htail_span=7.916667
htail_pos_lon=-16.083333
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=16.000000
vtail_span=4.560702
vtail_sweep=0.000000
vtail_pos_lon=-14.750000
vtail_pos_vert=4.166667
elevator_area=15.000000
aileron_area=11.740000
rudder_area=6.000000
elevator_up_limit=30.0		 	// was 25.000447
elevator_down_limit=18.998903
aileron_up_limit=17.996227
aileron_down_limit=13.000035
rudder_limit=20.995472
elevator_trim_limit=10.0 		// was 19.497754 
spoiler_limit=70
spoilerons_available=1			// was 0
aileron_to_spoileron_gain=0.0005	// was 0
min_ailerons_for_spoilerons=0.005	// was 0
min_flaps_for_spoilerons=0.005	// was 0

[GeneralEngineData]
engine_type=0
Engine.0=8.3
Engine.1=8.3 // 'dummy' for tail rotor
fuel_flow_scalar=1.00
min_throttle_limit=0.000000

[piston_engine]
power_scalar=1.0                    //Piston power scalar
cylinder_displacement=100.300000
compression_ratio=6.0
number_of_cylinders=6			// was 2
max_rated_rpm=3500			// was 2700
max_rated_hp=100.0 			// was 115
fuel_metering_type=1
cooling_type=0				// was 1
normalized_starter_torque=0.3
turbocharged=0
max_design_mp=0.0
min_design_mp=0.0
critical_altitude=0.0
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
thrust_scalar=1.0   			// Propeller thrust scalar
propeller_type=2				// was 0
propeller_diameter=8.000		// was 5.433000
propeller_blades=2
propeller_moi=20.50000			// was 3.350000
beta_max=29.800000
beta_min=4.000000				// was 17.000000 
min_gov_rpm=50.000000			// was 700.000000
prop_tc=0.4					// was 0.004000
gear_reduction_ratio=1.10		// was 1.0
fixed_pitch_beta=0
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=1
prop_auto_feathering_available=0
min_rpm_for_feather=0
beta_feather=90.0
power_absorbed_cf=0.0
defeathering_accumulators_available=0	// was 1
prop_reverse_available=1			// was 0
minimum_on_ground_beta=2.0			// was 0
minimum_reverse_beta=0.000000

[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=500.000000		// was 700
autothrottle_available=0
pitch_takeoff_ga=-5.00				// was 8.0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[direction_indicators]
direction_indicator.0=1,0

[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=15.996982
flap_limit_idle=0.000000
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0