// Pacific Pilot AI Boat
// by Jon Patch © 2005 
//
// based on boat framework by Winfried Orthmann
// Assistance from Holger Sandmann and Lou (Firestriker)
// Pilot Boat configuration files : © 2005 Ken Peters © Larry Robinson
// Floatplane effects by Holger Sandmann
//
// March 2005
//
// !!!Copyright remains with the original authors!!!


[fltsim.0]
title=Pacific Pilot
sim=pacific_pilot
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=AI Vessel
ui_type=Pacific Pilot
ui_variation=
description=           



[General]
atc_type=Boat
atc_model=Pilot
editable=1
performance= \n \n \n \n \n \n \n
Category=airplane



[contact_points]
//---- misc tweaked parameters 

//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,  7.00,  4.25, -1.20, 13574.8, 2, 0.519, 9.000, 0.800, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000
point.1=1, -7.00, -4.25, -1.20, 13574.8, 0, 0.519, 9.000, 0.800, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000
point.2=1, -7.00,  4.25, -1.20, 13574.8, 0, 0.519, 9.000, 0.800, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000
point.3=1,  7.00, -4.25, -1.20, 13574.8, 1, 0.519, 9.000, 0.800, 2.500, 0.700, 0.000, 0.000, 1.000, 0.000, 0.000

//point.0=4, 26, -3, -0.5, 9999, 0, 1, 10, 0.9, 15.5, 0.65, 00, 00, 2, 00, 00
//point.1=4, 26,  3, -0.5, 9999, 0, 1, 10, 0.9, 15.5, 0.65, 00, 00, 3, 00, 00
//point.2=4,-31, -5, -0.5, 9999, 0, 1, 10, 0.9, 15.5, 0.65, 00, 00, 2, 00, 00
//point.3=4,-31,  5, -0.5, 9999, 0, 1, 10, 0.9, 15.5, 0.65, 00, 00, 3, 00, 00

static_pitch=-0.000000
static_cg_height=1.500000


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0=1,   5.90,   0.00,  27.80, fx_navwhi ,
light.1=1,  14.50,  -6.00,   9.00, fx_navredh ,
light.2=1,  14.50,   6.00,   9.00, fx_navgreh ,
light.3=1,   0.00,  -5.00,  -2.00, fx_AI_floatplane_spray-and-wake
light.4=1,   0.00,   5.00,  -2.00, fx_AI_floatplane_spray-and-wake


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


[WEIGHT_AND_BALANCE]
max_gross_weight=2500                         // (pounds)
empty_weight=2500                             // (pounds)

reference_datum_position=0, 0, 0       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=170, -3.0, -1.5, 0.0           //Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170, -3.0,  1.5, 0.0           //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=0, -6.2, -1.5, 0.0           //Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=0, -6.2,  1.5, 0.0           //Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=0, -8.0,  0.0, 0.0           //Baggage         Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI=25400.0
empty_weight_roll_MOI=27137.0
empty_weight_yaw_MOI=2000.00 //20060.0  // high values cause poorly damped yaw oscillation. // without this change, other changes are not effective.
//CG_forward_limit=0.000000
//CG_aft_limit=1.000000
empty_weight_coupled_MOI=1.0 //100.000000  // no particular reason to couple moi in this case. 


[piston_engine]
power_scalar=2.0                              //Piston power scalar
//power_scalar=1.0                              //Piston power scalar
cylinder_displacement=90.3                     //Cubic inches per cylinder
compression_ratio=8.5                          //Compression ratio
number_of_cylinders=4                          //Number of cylinders
max_rated_rpm=3500                             //Max rated RPM
max_rated_hp=150                              //Max rated HP
//max_rated_hp=60                              //Max rated HP
fuel_metering_type=0                           //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type=1                                //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3                  //Starter torque factor
turbocharged=1                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=50                                //Max design manifold pressure, (inHg)
min_design_mp=0                                //Min design manifold pressure, (inHg)
critical_altitude=12500                            //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0                  //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar=0.4                 //Scalar on idle RPM friction


[airplane_geometry]
wing_area=20.0 //2.39000000  // experiment related to heeling; no effect, but kept new value
wing_span=8.6083333
//wing_area=239.000000
//wing_span=86.083333
wing_root_chord=4.916670
wing_tip_chord=4.916670
wing_dihedral=-0.735840  
wing_incidence=-19.499634
wing_twist=0.999268
oswald_efficiency_factor=0.0308470
//oswald_efficiency_factor=0.708470
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=6.0
wing_pos_apex_vert=35.000000
htail_area=9.000000
htail_span=11.666667
htail_pos_lon=-18.266667
htail_pos_vert=0.000000
htail_incidence=19.246460
htail_sweep=0.000000
vtail_area=9.0 //900.000000  // suspect this extreme value was an attempt to cure wigwag.
vtail_pos_lon=-176.183333
vtail_pos_vert=0.000000
elevator_area=16.610000
aileron_area=1.300000
rudder_area= 1.0 //300.650000 // suspect this was also an attempt to cure wigwag. 
elevator_up_limit=28.000447
elevator_down_limit=20.998903
aileron_up_limit=19.996227
aileron_down_limit=15.000035
rudder_limit=10.0 //3.995472
elevator_trim_limit=19.497754
spoiler_limit=45.000000
vtail_span=4.837355
vtail_sweep=0.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
auto_spoiler_available=0
spoiler_extension_time=0.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000



[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=19.9
induced_drag_scalar=19.9
elevator_effectiveness=0.1
aileron_effectiveness=0.05  //0.1
rudder_effectiveness=0.05 //2.0  // note dramatic reduction // to prevent oversteer
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0 //4.0  // questionable effect
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[propeller]
thrust_scalar=1.0                             //Propeller thrust scalar
propeller_type=1                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=6.7                         //Propeller Diameter, (feet)
propeller_blades=2                             //Number of propeller blades
propeller_moi=8.7                              //Propeller moment of inertia
beta_max=31.8                                  //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=17.0                                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1400                               //Miminum governed RPM
prop_tc=0.1                                    //Prop time-constant
gear_reduction_ratio=1.0                       //Propeller gear reduction ratio
fixed_pitch_beta=20                            //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=0                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=0                          //Minimum RPM for prop feathering
beta_feather=0                                 //Feathering pitch angle (degrees)
power_absorbed_cf=0                            //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available=0                       //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=0                       //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0                         //Minimum pitch angle in reverse, (degrees)

[electrical]
//electric_always_available=0

[Views]
//eyepoint=-4.3, -2.8,3.1       //(feet) longitudinal, lateral, vertical distance from reference datum
eyepoint=3.6, 0.0, 1.6
//eyepoint=-3.433395,-0.192237,0.333210
//eyepoint=-3.946026,-2.768209,3.050156

[SMOKESYSTEM]
//smoke.0=0.0, -6.0, -2.40, fx_exhaust

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=0
Com.1=1, 0
Nav.1=0, 0, 0
Adf.1=0
Transponder.1=0
Marker.1=0

[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=1,0

//[fuel]
//Center1=-2.6,  0.0,  0.0, 11.1, 0.0    
//fuel_type=1.000000
//number_of_tank_selectors=1

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=6.800000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=60.0,0.000000
flaps-position.2=90.0,0.000000
lift_scalar=0.001
drag_scalar=2.0
pitch_scalar=26.000

[GeneralEngineData]
engine_type=0
Engine.0=0.400000,0.000000,-19.200000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
autoland_available=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

[fuel]
LeftMain=-3.600000,0.000000,0.000000,20.000000,0.000000
//RightMain=-3.600000,0.000000,0.000000,20.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0

[exits]
number_of_exits=2
exit_rate.0=1.0   
exit_rate.1=1.0 

[Reference Speeds]
flaps_up_stall_speed=54.000000
full_flaps_stall_speed=43.200000
cruise_speed=31.347075
max_indicated_speed=180.000000

[brakes]
toe_brakes_scale=0.000000
parking_brake=0

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1
stick_shaker=0

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[forcefeedback]
gear_bump_nose_magnitude=6000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=1000           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=1250000          ; in microseconds
gear_bump_right_magnitude=6000          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=250             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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
[pitot_static]
pitot_heat=0.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=0
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0
