// AI Helicopter configuration files
// by Rob Nieuwenhoven based on the work of Holger Sandmann // (hsandman@sfu.ca)
// and Doug Callihan
//
// Version 1, May 2004
//
// for GMAX As350 Ecureuil
// by Tamas Nemeth and Peter Nemeth (pencee@vnet.hu)
//
// 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=AI AS 350 Ecureuil Eurocopter
sim=stemme_as_helicopter_2
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
prop_anim_ratio=-0.72
//prop_anim_ratio=-1.86
atc_id=AS-350
description=The AS.350 was developed by Aerospatiale in the early 1970s, an Avco Lycoming powered prototype first flying on 27 June 1974, followed by a Turbomeca Arriel version on 14 February 1975. Customer deliveries of the Ecureuil (Squirrel) began in April 1978.\nThe Ecureuil was intended to replace the Alouette, and to compete with the Bell 206. The type represents one of Europe's most successful civil helicopter designs, and has found numerous overseas markets. It was also produced as the AS.550 Fennec military helicopter.\n
atc_heavy=0
atc_airline=
atc_flight_number=350
atc_parking_codes=
atc_parking_types=RAMP
[fltsim.1]
title=AI AS 350 Ecureuil AIR ZERMATT
sim=stemme_as_helicopter_2
model=
panel=
sound=
texture=airzermatt
kb_checklists=
kb_reference=
prop_anim_ratio=-0.72
//prop_anim_ratio=-1.86
atc_id=HB-XSU
description=The AS.350 was developed by Aerospatiale in the early 1970s, an Avco Lycoming powered prototype first flying on 27 June 1974, followed by a Turbomeca Arriel version on 14 February 1975. Customer deliveries of the Ecureuil (Squirrel) began in April 1978.\nThe Ecureuil was intended to replace the Alouette, and to compete with the Bell 206. The type represents one of Europe's most successful civil helicopter designs, and has found numerous overseas markets. It was also produced as the AS.550 Fennec military helicopter.\n
atc_heavy=0
atc_airline=
atc_flight_number=350
atc_parking_codes=
atc_parking_types=RAMP
[fltsim.2]
title=AI AS 350 Ecureuil HB-XJB Airport Helicopter
sim=stemme_as_helicopter_2
model=
panel=
sound=
texture=airport
kb_checklists=
kb_reference=
prop_anim_ratio=-0.72
//prop_anim_ratio=-1.86
atc_id=HB-XJB
description=The AS.350 was developed by Aerospatiale in the early 1970s, an Avco Lycoming powered prototype first flying on 27 June 1974, followed by a Turbomeca Arriel version on 14 February 1975. Customer deliveries of the Ecureuil (Squirrel) began in April 1978.\nThe Ecureuil was intended to replace the Alouette, and to compete with the Bell 206. The type represents one of Europe's most successful civil helicopter designs, and has found numerous overseas markets. It was also produced as the AS.550 Fennec military helicopter.\n
atc_heavy=0
atc_airline=
atc_flight_number=XJB
atc_parking_codes=
atc_parking_types=RAMP
[fltsim.3]
title=AI AS 350 Ecureuil N10BC
sim=stemme_as_helicopter_2
model=
panel=
sound=
texture=cnbc
kb_checklists=
kb_reference=
prop_anim_ratio=-0.72
//prop_anim_ratio=-1.86
atc_id=N10BC
description=The AS.350 was developed by Aerospatiale in the early 1970s, an Avco Lycoming powered prototype first flying on 27 June 1974, followed by a Turbomeca Arriel version on 14 February 1975. Customer deliveries of the Ecureuil (Squirrel) began in April 1978.\nThe Ecureuil was intended to replace the Alouette, and to compete with the Bell 206. The type represents one of Europe's most successful civil helicopter designs, and has found numerous overseas markets. It was also produced as the AS.550 Fennec military helicopter.\n
atc_heavy=0
atc_airline=
atc_flight_number=350
atc_parking_codes=
atc_parking_types=RAMP
[fltsim.4]
title=AI AS 350 Ecureuil G-LHPL
sim=stemme_as_helicopter_2
model=
panel=
sound=
texture=glhpl
kb_checklists=
kb_reference=
prop_anim_ratio=-0.72
//prop_anim_ratio=-1.86
atc_id=G-LHPL
description=The AS.350 was developed by Aerospatiale in the early 1970s, an Avco Lycoming powered prototype first flying on 27 June 1974, followed by a Turbomeca Arriel version on 14 February 1975. Customer deliveries of the Ecureuil (Squirrel) began in April 1978.\nThe Ecureuil was intended to replace the Alouette, and to compete with the Bell 206. The type represents one of Europe's most successful civil helicopter designs, and has found numerous overseas markets. It was also produced as the AS.550 Fennec military helicopter.\n
atc_heavy=0
atc_airline=
atc_flight_number=350
atc_parking_codes=
atc_parking_types=RAMP
[General]
performance=AS-350 - One 546kW (732shp) Turboméca Arriel 1D1 turboshaft driving a three blade main rotor and two blade tail rotor.\nMax speed 287km\/h (155kt), cruise speed 242km\/h (131kt). Max rate of climb 1752ft\/min. Hovering ceiling out of ground effect 8360ft. Range with max fuel 772km (448nm). \n
atc_model=AS350 SQUIRREL
atc_type=Aerospatiale
editable=1
[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=110
max_indicated_speed=180.000000
[flight_tuning]
cruise_lift_scalar=1.20 // 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
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=cabin
light.0 = 3, -15.74, -4.25, 0.04, fx_navred ,
light.1 = 3, -15.74, 4.25, 0.04, fx_navgre ,
light.2 = 3, -23.62, 0.00, 0.49, fx_navwhi ,
light.3 = 1, -23.95, 0.00, 5.24, fx_beacon ,
light.4 = 5, 5.50, 1.16, -3.75, fx_landing ,
light.5 = 5, 5.50, -1.16, -3.75, fx_landing ,
light.6 = 4, 6.23, 0.00, 0.50, fx_vclighth ,
light.7 = 10, 3.28, 0.00, 0.50, fx_vclight ,
light.8 = 2, -15.74, -4.25, 0.04, fx_strobe ,
light.9 = 2, -15.74, 4.25, 0.04, fx_strobe ,
light.10 = 2, -23.62, 0.00, 0.49, fx_strobe ,
[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
[exits]
number_of_exits=2
exit_rate.0=0.4
exit_rate.1=0.4
[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
[Views]
eyepoint=6.230, 1.200, 0.940
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[airspeed_indicators]
airspeed_indicator.0=1,7
//---- parameters from AS350, 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, 5.570, 3.600, -6.000, 1574.000, 0.000, 0.980, 0.000, 0.280, 2.500, 0.680, 0.000, 0.000, 7.000, 0.000, 0.000
point.1= 1, 5.570, -3.600, -6.000, 1574.000, 0.000, 0.980, 0.000, 0.280, 2.500, 0.680, 0.000, 0.000, 7.000, 0.000, 0.000
point.2= 1, -4.590, 3.600, -6.000, 1574.000, 0.000, 0.980, 0.000, 0.390, 2.500, 0.700, 0.000, 0.000, 8.000, 0.000, 0.000
point.3= 1, -4.590, -3.600, -6.000, 1574.000, 0.000, 0.980, 0.000, 0.390, 2.500, 0.700, 0.000, 0.000, 8.000, 0.000, 0.000
//point.0= 3.000, 5.570, 3.600, -6.000, 1574.000, 0.000, 0.980, 0.000, 0.280, 2.500, 0.680, 0.000, 0.000, 7.000, 0.000, 0.000
//point.1= 3.000, 5.570, -3.600, -6.000, 1574.000, 0.000, 0.980, 0.000, 0.280, 2.500, 0.680, 0.000, 0.000, 7.000, 0.000, 0.000
//point.2= 3.000, -4.590, 3.600, -6.000, 1574.000, 0.000, 0.980, 0.000, 0.390, 2.500, 0.700, 0.000, 0.000, 8.000, 0.000, 0.000
//point.3= 3.000, -4.590, -3.600, -6.000, 1574.000, 0.000, 0.980, 0.000, 0.390, 2.500, 0.700, 0.000, 0.000, 8.000, 0.000, 0.000
//point.4= 2.000, 0.000, -16.730, 4.420, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
//point.5= 2.000, 0.000, 16.730, 4.420, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
//point.6= 2.000, -24.270, 0.000, 4.920, 300.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
//point.7= 2.000, 16.730, 0.000, 4.420, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
//point.8= 2.000, 11.480, 0.000, -1.960, 300.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
//point.9= 2.000, -24.270, 0.000, -2.620, 500.000, 0.000, 0.000, 0.000, 0.250, 1.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
static_pitch = 0.200
static_cg_height = 6.000
//---- 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
[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
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=0
