// AI Vessel configuration files
// by Holger Sandmann, hsandman@telus.ca
// FS9 Version, July 2005
//
// for Alaska Marine Highway Ferry MV Matanuska
// by Mitsuya Hamaguchi ("hama"), m28hama@i.bekkoame.ne.jp
//
// !!!Copyright remains with the original author!!!

[fltsim.0]
title=AI Vessel MV Matanuska TF
sim=hama_leconte
model=
panel=
sound=
texture=Matanuska
kb_checklists=
kb_reference=
atc_id_color=
atc_id=
atc_airline=
atc_flight_number=
atc_parking_types=DOCK
ui_manufacturer=AI Vessel
ui_type=Alaska Ferries
ui_variation=MV Matanuska
description=Copyright by Mitsuya Hamaguchi (hama) \ http//f1.aaacafe.ne.jp/~rjnnhama/craft.htm/              


[General]
atc_type=AI AMHS Ferry
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)

// Class 1 points provide the main ground contact
point.0=1,  -1.00,  4.25, -3.500, 13574.8, 2, 0.519, 1.000, 0.900, 2.500, 0.700, 0.0, 0.0, 0.0, 0.0, 0.0
point.1=1, -25.20, -4.25, -3.500, 13574.8, 0, 0.519, 1.000, 0.900, 2.500, 0.700, 0.0, 0.0, 2.0, 0.0, 0.0
point.2=1, -25.20,  4.25, -3.500, 13574.8, 0, 0.519, 1.000, 0.900, 2.500, 0.700, 0.0, 0.0, 3.0, 0.0, 0.0
point.3=1,  -1.00, -4.25, -3.500, 13574.8, 1, 0.519, 1.000, 0.900, 2.500, 0.700, 0.0, 0.0, 1.0, 0.0, 0.0

// Class 4 points determine the trigger points for splash effects
point.4=4, -13.10,  0.00, -3.400, 13574.8, 0, 0.319, 1.000, 0.900, 2.500, 0.700, 0.0, 0.0, 0.0, 0.0, 0.0

//original
//point.0=4,8.0, -4.00, -2.80, 9900, 0, 1.40, 0, 0.8,12.5, 0.70, 0.0, 0.0, 0, 0.0, 0.0
//point.1=4,8.0,  4.00, -2.80, 9900, 0, 1.40, 0, 0.8,12.5, 0.70, 0.0, 0.0, 0, 0.0, 0.0
//point.2=1,-10.0, 0.00, -2.670, 9900, 0, 1.40, 0, 0.8,12.5, 0.70, 0.0, 0.0, 0, 0.0, 0.0


max_number_of_points=21

static_pitch=0.000             //degrees, pitch when at rest on the ground (+=Up, -=Dn)
//static_pitch=-0.000          
static_cg_height=3.5           //feet, altitude of CG when at rest on the ground
static_cg_height=3.0       
gear_system_type=1             //Hydraulic


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit            
light.0=1,  29.00,   0.00,  80.50, fx_navwhi ,
light.1=1,  93.80, -35.99,  41.50, fx_navredm ,
light.2=1,  93.80,  35.99,  41.50, fx_navgrem ,
light.3=1,  90.90,   0.00,  58.20, fx_beaconh ,
light.5=1, 188.00,   0.00,  34.00, fx_navwhi ,
light.6=1,-200.80,   0.00,  40.70, fx_navwhi ,
//light.7=1, 170.00,   0.00,  -3.50, MF_AI_ship_wake_Matanuska

//light.0=3, 43.00,   0.00, 81.50, fx_navwhih ,
//light.1=3, 108.00, -36.10, 41.50,  fx_navredm ,
//light.2=3, 108.00,  36.10, 41.50, fx_navgrem ,
//light.3=1, 48.00,   0.00, 75.00,  fx_beaconh ,
//light.4=3, 199.0,   0.00, 34.00, fx_navwhih ,
//light.5=3, -188.0,   0.00, 42.00, fx_navwhih ,
//light.6=1, 20.00,  0.00,  -5.60, MF_AI_ship_wake_xl


[SMOKESYSTEM]
smoke.0=0, -37.5, 0.0, fx_Smoke_seikan.fx,
smoke.1=0, -119.5, 7.0, fx_spray1.fx,
smoke.2=0, -119.5, -7.0, fx_spray1.fx,


[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=MF_AI_ship_Matanuska
touchdown=fx_tchdwn_s, 1

//wake=fx_wake_m
//water=fx_spray_leconte
//dirt=fx_tchdrt
//concrete=fx_sparks
//touchdown=fx_tchdwn_s, 1

[BRAKES]
toe_brakes_scale=0.000000
parking_brake=0


[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, Pilot"              // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.1="170.0,  -11.3,  1.5,   0.0, Passenger 1"        // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.2="160.0,  -13.9, -2.0,   0.0, Passenger 2]"        // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.3="160.0,  -13.9,  2.0,   0.0, Passenger 3"        // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.4="0.0,  -18.8, -2.0,   0.0, Passenger 4"        // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.5="0.0,  -18.8,  2.0,   0.0, Passenger 5"        // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.6=" 50.0,  -21.0,  0.0,   0.0, "       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.7="25.0,  -23.5,  0.0,   0.0, "       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.8="0.0,  -25.6,  0.0,   0.0, "       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.9="0.0,  -27.5,  0.0,   0.0, "       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.10="0.0,   -9.9, -5.3,  -6.5, "       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.11="0.0,   -9.9,  5.3,  -6.5, "      // 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              //Square feet
wing_span=8.6083333               //Feet
//wing_area=279.0
//wing_span=52.1                  
wing_root_chord=6.4               //Feet
wing_dihedral=3.9                 //Degrees
wing_incidence=2.5                //Degrees
wing_twist=-1.7                   //Degrees
oswald_efficiency_factor=0.03
//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=0.01			    //Scalar on Turboprop power
//power_scalar=1.0                
maximum_torque=1865               //Maximum torque available (ft-lbs)


[propeller]
thrust_scalar=0.01                //Propeller thrust scalar
//thrust_scalar=1.0               
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)




//---- unchanged parameters based on air file

[fuel]
LeftMain=-15.300000,-1.100000,2.500000,166.000000,3.600000
RightMain=-15.300000,1.100000,2.500000,166.000000,3.600000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=1
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=7.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=12.666187,0.000000
flaps-position.2=25.332374,0.000000
flaps-position.3=37.998561,0.000000
[GeneralEngineData]
engine_type=5
Engine.0=-1.266667,4.166667,0.000000
Engine.1=-1.266667,-4.166667,0.000000
fuel_flow_scalar=1.000000
min_throttle_limit=-0.349915
[TurbineEngineData]
fuel_flow_gain=0.011000
inlet_area=1.000000
rated_N2_rpm=33000.000000
static_thrust=158.000000
afterburner_available=0
[Reference Speeds]
flaps_up_stall_speed=66.000000
full_flaps_stall_speed=52.800000
cruise_speed=69.034805
max_indicated_speed=180.000000
max_mach=1.000000
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[Views]
eyepoint=-13.100000,0.000000,0.000000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
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
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=3,0
