// AI Vessel configuration files
// by Holger Sandmann, hsandman@sfu.ca
// FS9 Version, January 2004
//
// for Cruise Ship Asuka
// by Mitsuya Hamaguchi ("hama"), m28hama@i.bekkoame.ne.jp
//
// !!!Copyright remains with the original authors!!!
[fltsim.0]
title=AI Cruise Ship Asuka
sim=hama_asuka
model=asuka
panel=
sound=
texture=asuka
kb_checklists=
kb_reference=
atc_id_color=0xff000000
atc_id=N208EH
atc_airline=
atc_flight_number=
atc_parking_types=
ui_manufacturer=AI Vessel
ui_type=Cruise Ship
ui_variation=asuka
description=\n \n\n \n\n \n
[General]
atc_type=
atc_model=
performance=\n\n
//---- misc tweaked parameters
[contact_points]
//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)
point.0=4, -4.00, 2.00, -5.000, 13574.8, 0, 0.319, 0.000, 0.900, 2.500, 0.700, 0.0, 0.0, 0.0, 0.0, 0.0
point.1=4, -26.35, -2.00, -5.000, 13574.8, 0, 0.319, 0.000, 0.900, 2.500, 0.700, 0.0, 0.0, 2.0, 0.0, 0.0
point.2=4, -26.35, 2.00, -5.000, 13574.8, 0, 0.319, 0.000, 0.900, 2.500, 0.700, 0.0, 0.0, 3.0, 0.0, 0.0
point.3=4, -4.00, -2.00, -5.000, 13574.8, 0, 0.319, 0.000, 0.900, 2.500, 0.700, 0.0, 0.0, 1.0, 0.0, 0.0
point.4=1, -1.15, 4.25, -5.800, 13574.8, 2, 0.519, 9.000, 0.900, 2.500, 0.700, 0.0, 0.0, 0.0, 0.0, 0.0
point.5=1, -16.40, -4.25, -5.800, 13574.8, 0, 0.519, 9.000, 0.900, 2.500, 0.700, 0.0, 0.0, 2.0, 0.0, 0.0
point.6=1, -16.40, 4.25, -5.800, 13574.8, 0, 0.519, 9.000, 0.900, 2.500, 0.700, 0.0, 0.0, 3.0, 0.0, 0.0
point.7=1, -1.15, -4.25, -5.800, 13574.8, 1, 0.519, 9.000, 0.900, 2.500, 0.700, 0.0, 0.0, 1.0, 0.0, 0.0
//point.0=4, 15.98, 2.00, -5.600, 13574.8, 0, 0.319, 0.000, 0.800, 2.500, 0.700, 0.0, 0.0, 0.0, 0.0, 0.0
//point.1=4, -18.48, -2.00, -5.600, 13574.8, 0, 0.319, 0.000, 0.800, 2.500, 0.700, 0.0, 0.0, 2.0, 0.0, 0.0
//point.2=4, -18.48, 2.00, -5.600, 13574.8, 0, 0.319, 0.000, 0.800, 2.500, 0.700, 0.0, 0.0, 3.0, 0.0, 0.0
//point.3=4, 15.98, -2.00, -5.600, 13574.8, 0, 0.319, 0.000, 0.800, 2.500, 0.700, 0.0, 0.0, 1.0, 0.0, 0.0
//point.4=1, 7.00, 4.25, -5.800, 13574.8, 2, 0.519, 9.000, 0.800, 2.500, 0.700, 0.0, 0.0, 0.0, 0.0, 0.0
//point.5=1, -7.00, -4.25, -5.800, 13574.8, 0, 0.519, 9.000, 0.800, 2.500, 0.700, 0.0, 0.0, 2.0, 0.0, 0.0
//point.6=1, -7.00, 4.25, -5.800, 13574.8, 0, 0.519, 9.000, 0.800, 2.500, 0.700, 0.0, 0.0, 3.0, 0.0, 0.0
//point.7=1, 7.00, -4.25, -5.800, 13574.8, 1, 0.519, 9.000, 0.800, 2.500, 0.700, 0.0, 0.0, 1.0, 0.0, 0.0
//point.0=1, -1.15, -5.250, -7.800, 1600, 0, 1.40, 30.0, 0.3, 2.5, 0.8, 4.0, 4.0, 0, 175.0, 175.0
//point.1=1, -1.15, 5.250, -7.800, 1600, 0, 1.40, 30.0, 0.3, 2.5, 0.8, 4.0, 4.0, 1, 175.0, 175.0
//point.2=1, -16.40, -5.250, -7.700, 1600, 1, 1.50, 0.0, 0.4, 2.5, 0.8, 4.0, 4.0, 2, 175.0, 175.0
//point.3=1, -16.40, 5.250, -7.700, 1600, 2, 1.50, 0.0, 0.4, 2.5, 0.8, 4.0, 4.0, 3, 175.0, 175.0
//point.4=4, -4.00, -5.250, -5.600, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 0, 0.0, 0.0
//point.5=4, -4.00, 5.250, -5.600, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 1, 0.0, 0.0
//point.6=4, -26.35, -5.250, -5.600, 1600, 0, 0.00, 0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 2, 0.0, 0.0
//point.7=4, -26.35, 5.250, -5.600, 1600, 0, 0.00, 0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 3, 0.0, 0.0
//point.8=2, -12.90, -26.00, 3.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
//point.9=2, -12.90 26.00, 3.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
//point.10=2, -36.23, 0.00, 0.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
//point.11=2, -0.50, 0.00, -2.17, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
//point.12=2, -38.00, 0.00, 9.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7, 0.0, 0.0
//point.13=5, -30.90, -5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.0, 1.0, 1.2, 0, 0.0, 0.0
//point.14=5, -30.90, 5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.0, 1.1, 1.5, 0, 0.0, 0.0
max_number_of_points=21
static_pitch=0.000
//static_pitch=0.983 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=6.344 //feet, altitude of CG when at rest on the ground
//static_cg_height=7.344 //feet, altitude of CG when at rest on the ground
gear_system_type=1 //Hydraulic
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=1, -275.22, 0.00, 58.54, fx_navwhih
light.1=1, 195.00, -41.28, 84.02, asuka_fx_navred
light.2=1, 195.00, 41.28, 84.02, asuka_fx_navgrem
light.3=1, 183.20, 0.00, 113.15, fx_beacon
light.4=1, 350.62, 0.00, 51.72, fx_navwhi
light.5=1, 250.00, -23.00, -5.60, fx_AI_ship_wake_xl
light.6=1, 250.00, 23.00, -5.60, fx_AI_ship_wake_xl
light.7=1, -240.00, -20.00, -5.80, fx_AI_ship_trail-of-spray
light.8=1, -240.00, 20.00, -5.80, fx_AI_ship_trail-of-spray
light.9=1, 283.00, 0.00, -5.60, fx_spray
light.10=1, -70.00, 0.00, 0.00, fx_smoke_ship
light.11=1, -64.00, 0.00, 113.00, fx_beaconh
light.12=1, 86.00, 0.00, 125.00, fx_navwhi
[SMOKESYSTEM]
smoke.0=0, -70, 0.0, fx_smoke_ship,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
//wake=fx_wake_m
//water=fx_spray1
//dirt=fx_tchdrt
//concrete=fx_sparks
//touchdown=fx_tchdwn_s, 1
[brakes]
parking_brake=1 //Parking brake available
toe_brakes_scale=0.068 //Brake scalar
[WEIGHT_AND_BALANCE]
max_gross_weight=8000 // (pounds)
empty_weight=4895 // (pounds)
reference_datum_position=13.1, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-13.6, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
//station_load.0="170.0, -11.3, -1.5, 0.0, pCbg" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.1="170.0, -11.3, 1.5, 0.0, æq 1" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.2="160.0, -13.9, -2.0, 0.0, æq 2]" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.3="160.0, -13.9, 2.0, 0.0, æq 3" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.4="0.0, -18.8, -2.0, 0.0, æq 4" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.5="0.0, -18.8, 2.0, 0.0, æq 5" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.6=" 50.0, -21.0, 0.0, 0.0, ݨXy[X 1" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.7="25.0, -23.5, 0.0, 0.0, ݨXy[X 2" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.8="0.0, -25.6, 0.0, 0.0, ݨXy[X 3" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.9="0.0, -27.5, 0.0, 0.0, ݨXy[X 4" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.10="0.0, -9.9, -5.3, -6.5, ¶¤Ìèר" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.11="0.0, -9.9, 5.3, -6.5, E¤Ìèר" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI=7241.36
empty_weight_roll_MOI=5618.57
empty_weight_yaw_MOI=10431.43
empty_weight_coupled_MOI=0.0
[airplane_geometry]
wing_area=2.39000000
wing_span=8.6083333
//wing_area=279.0 //Square feet
//wing_span=52.1 //Feet
wing_root_chord=6.4 //Feet
wing_dihedral=3.9 //Degrees
wing_incidence=2.5 //Degrees
wing_twist=-1.7 //Degrees
oswald_efficiency_factor=0.0308470
//oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=2.96 //Degrees, wing leading edge
wing_pos_apex_lon=-12.3 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_area=39.0 //Square feet
htail_span=11.7 //Feet
htail_pos_lon=-27.8 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence=2.0 //Degrees
htail_sweep=5.0 //Degrees, horizontal tail leading edge
vtail_area=18.0 //Square feet
vtail_span=4.8 //Feet, tip to body
vtail_sweep=45.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-25.7 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=1.5 //Feet, vertical distance from reference point, positive going up
elevator_area=16.6 //Square feet
aileron_area=18.3 //Square feet
rudder_area=6.6 //Square feet
elevator_up_limit=28.0 //Degrees
elevator_down_limit=21.0 //Degrees
aileron_up_limit=20.0 //Degrees
aileron_down_limit=15.0 //Degrees
rudder_limit=15.5 //Degrees
elevator_trim_limit=19.5 //Degrees
spoiler_limit=20.0 //Degrees
spoilerons_available=1 //Spoilerons Available?
aileron_to_spoileron_gain=1 //Aileron to spoileron gain
min_ailerons_for_spoilerons=0 //Degrees
min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate
spoiler_handle_available=0 //Defaults to True if spoiler limit > 0, else False. Should be False for spoilerons only
[turboprop_engine]
power_scalar=1.0 //Scalar on Turboprop power
maximum_torque=1865 //Maximum torque available (ft-lbs)
//---- original parameters from Cruise Ship Asuka
[Flaps.0]
type=1
span-outboard=0.5 // Percent span for flap position
extending-time=5.7 // Seconds, time to fully extend
system_type=0 // 0 = electrical
damaging-speed=175 // KIAS
blowout-speed=175 // KIAS
flaps-position.0=0 // degrees
flaps-position.1=10,175 // degrees
flaps-position.2=20,150 // degrees
flaps-position.3=30,125 // degrees
[flight_tuning]
cruise_lift_scalar=0
parasite_drag_scalar=0
induced_drag_scalar=0
elevator_effectiveness=0
aileron_effectiveness=0
rudder_effectiveness=1.0
pitch_stability=0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=0
aileron_trim_effectiveness=0
rudder_trim_effectiveness=1.0
[GeneralEngineData]
engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-1.3, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.12 //Scalar for fuel flow efficiency
min_throttle_limit=-0.25 //Minimum percent throttle. Generally negative for turbine reverser
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=8.8 //Propeller Diameter, (feet)
propeller_blades=3 //Number of propeller blades
propeller_moi=19 //Propeller moment of inertia
beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=15.6 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25520 //Miminum governed RPM
prop_tc=0.004 //Prop time-constant
gear_reduction_ratio=17.4 //Propeller gear reduction ratio
fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=700 //Minimum RPM for prop feathering
beta_feather=88.0 //Feathering pitch angle (degrees)
power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees)
[TurbineEngineData]
fuel_flow_gain=0.011 //Gain on fuel flow
inlet_area=1.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm=33000 //RPM, second stage compressor rated value
static_thrust=158 //Lbs, max rated static thrust at Sea Level
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 5 , 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 2 , 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0
[gear_warning_system]
gear_warning_available=2 //Amphib
pct_throttle_limit=0.1 //Percent throttle that activates warning
flap_limit_idle=20.1 //Flap angle that activates warning at idle
flap_limit_power=13.0 //Flap angle that activates warning at above idle
[hydraulic_system]
normal_pressure=3000.0 //PSI
electric_pumps=0 //no electric pumps
engine_map=1,0,0,0 //pump on Eng1
[Views]
eyepoint=226.5, -16.00,87.7 //(feet) longitudinal, lateral, vertical distance from reference datum
[Radios]
;/ Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1
[keyboard_response]
;/Breakpoint speeds (knots) on the keyboard increments of control surfaces.
;/Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator=100, 180
aileron=200, 1000
rudder=200, 1000
[direction_indicators]
;/1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
;/2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0
[attitude_indicators]
;/Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0=1
[turn_indicators]
;/Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,0
[airspeed_indicators]
airspeed_indicator.0=1.16, -22.0
[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4 ;Percent per second
[fuel]
LeftMain=-15.3, -1.1, 2.5, 166.0, 3.6 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-15.3, 1.1, 2.5, 166.0, 3.6 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=1
[Reference Speeds]
flaps_up_stall_speed=72.0 //Knots True (KCAS)
full_flaps_stall_speed=58.0 //Knots True (KCAS)
cruise_speed=143.0 //Knots True (KTAS)
max_mach=0.60
max_indicated_speed=175 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.0
autothrottle_available=0
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.0
[forcefeedback]
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000 ; 0 - 10000
crash_direction1=01000 ; 0 - 35999 degrees
crash_magnitude2=10000 ; 0 - 10000
crash_direction2=9000 ; 0 - 35999 degrees
crash_period2=75000 ; in microseconds
crash_duration2=2500000 ; in microseconds
[stall_warning]
type=2
