;NIMITZ-CLASS CARRIER (AI VERSION)
;By Phil Crowther
;AI = changes for AI
;SOURCE
;SingleEngineProp.cfg
;SingleEngineProp.air
;aircraft.cfg for LibertyShip
[fltsim.0]
title=AI HMAS Melbourne
sim=Nimitz
model=
panel=
sound=
texture=AUS
ui_manufacturer=FS Shipyards AI
ui_type=HMAS Melbourne
ui_variation=Clear Decks
description=
[fltsim.1]
title=AI CVN Stennis
sim=Nimitz
model=
panel=
sound=
texture=USA
ui_manufacturer=FS Shipyards AI
ui_type=CVN Stennis
ui_variation=Clear Decks
description=
[fltsim.2]
title=AI HMAS Melbourne with F18
sim=Nimitz
model=F18
panel=
sound=
texture=AUS
ui_manufacturer=FS Shipyards AI
ui_type=HMAS Melbourne
ui_variation=with F18s
description=
[fltsim.3]
title=AI CVN Stennis with F18
sim=Nimitz
model=F18
panel=
sound=
texture=USA
ui_manufacturer=FS Shipyards AI
ui_type=CVN Stennis
ui_variation=with F18s
description=
[General]
atc_type=
atc_model=
editable=1
performance=Maximum Speed\t20 kts\nCruise Speed\t11 kts\nMaximum Range\t19,000 nm\nService Ceiling\t0 ft\nFuel Capacity\t12,500 barrels\nMax Gross Weight\t20 million lbs\nSeating\t\t81\nUseful Load\t18 million lbs\n
[Reference Speeds]
flaps_up_stall_speed = 54.000
full_flaps_stall_speed = 43.200
cruise_speed = 129.000
max_indicated_speed = 163.000000
[WEIGHT_AND_BALANCE]
max_gross_weight = 2550.000
empty_weight = 1650.000
reference_datum_position = 0.000, 0.000, 0.000
;distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0.000, 0.000, 0.000
;---Moments of Inertia using Liberty Ship dimensions
empty_weight_pitch_MOI = 396165.000
empty_weight_roll_MOI = 2767.000
empty_weight_yaw_MOI = 132326.000
empty_weight_coupled_MOI = 0.000
[contact_points]
; 0 Class (0 = None, 1 = Wheel, 2 = Scrape, 3 = Skid, 4 = Float, 5 = Water Rudder)
; 1 Longitudinal Position (feet) [BIGGER = SLOWER WAVE MOTION + NOSE PLOWS]
; 2 Lateral Position (feet) [BIGGER CREATES VIBRATION]
; 3 Vertical Position (feet) [MORE POSITIVE = LOWER]
; 4 Impact Damage Threshold (Feet Per Minute)
; 5 Brake Map (0=None, 1=Left, 2=Right) [N/A]
; 6 Wheel Radius (feet)
; 7 Steer Angle (degrees) [CHANGE THIS TO MAKE SHIP TURN FASTER]
; 8 Static Compression (feet) (0=rigid)
; 9 Max/Static Compression Ratio
;10 Damping Ratio/Water Rudder Effectiveness (0=Undamped, 1=Critically Damped)
;11 Extension Time (seconds) [N/A TO FIXED GEAR]
;12 Retraction Time (seconds) [N/A TO FIXED GEAR]
;13 Sound Type [WATER SOUND?]
;14 Airspeed limit for retraction (KIAS) [N/A TO FIXED GEAR]
;15 Airspeed that gear gets damage at (KIAS) [N/A TO FIXED GEAR]
; 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
; 0 Z X Y FPM BM WR SA SC Max DR ET RT SND RL GD
;---MODIFIED FOR AI
point.0= 4, 10,-05,-4.5, 9999, 0, 1, 0.0, 0.9, 15.5, 0.65, 00, 00, 2, 000, 000
point.1= 4, 10, 05,-4.5, 9999, 0, 1, 0.0, 0.9, 15.5, 0.65, 00, 00, 3, 000, 000
point.2= 1,-10, 00,-4.5, 9999, 0, 1, 0.0, 0.9, 15.5, 0.65, 00, 00, 2, 000, 000
;---
static_pitch = 0.000
static_cg_height = 4.000 ;[MUST BE POS #, OR FLIES INTO SPACE]
[Views]
;ZXY distance from reference datum (feet)
eyepoint = 12.50, 0.00, 43.25 ;flying deck
[LIGHTS]
;type, longitudinal, lateral, vertical distance from ref datum, name
;Light types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
;adjust these positions as you would for the [Views] section
;---internal (flying deck)
light.0 = 4, 14.18, 0.15, 42.600, fx_vclighth ;high panel/VC-lighting
light.1 = 4, 14.18, 0.15, 42.600, fx_vclight ;normal panel/VC-lighting
;---external
light.2 = 3, 0.000, -5.40, 57.000, fx_navred ;smokestack left
light.3 = 3, 0.000, 5.40, 57.000, fx_navgre ;smokestack right
light.4 = 3, 129.844, 0.00, 71.172, fx_navwhi ;foremast
light.5 = 3, 60.864, 0.00, 76.001, fx_navwhi ;mainmast
light.6 = 3, -109.309, 0.00, 75.982, fx_navwhi ;mizzenmast
light.7 = 3, -173.633, 0.00, 40.120, fx_navwhi ;flagstaff
[EFFECTS]
;---MODIFIED FOR AI
concrete = fx_AI_ship_wake_l ;wake
[flight_tuning]
cruise_lift_scalar = 1.000
parasite_drag_scalar = 25.000
induced_drag_scalar = 1.000
elevator_effectiveness = 1.000
aileron_effectiveness = 1.000
rudder_effectiveness = 1.000
pitch_stability = 1.000
roll_stability = 1.000
yaw_stability = 1.000
elevator_trim_effectiveness = 1.000
aileron_trim_effectiveness = 1.000
rudder_trim_effectiveness = 1.000
[airplane_geometry]
wing_area = 174.0 ;Square feet
wing_span = 36.1 ;Feet
wing_root_chord = 4.9 ;Feet
wing_dihedral = 1.7 ;Degrees
wing_incidence = 1.5 ;Degrees
wing_twist = -3.0 ;Degrees
oswald_efficiency_factor = 0.68 ;Lift effeciency of wing
wing_winglets_flag = 0 ;Are winglets available?
wing_sweep = 0 ;Degrees, wing leading edge
wing_pos_apex_lon = -2.4 ;Z Feet
wing_pos_apex_vert = 0.0 ;Y Feet
htail_area = 39.0 ;Square feet
htail_span = 11.7 ;Feet
htail_pos_lon = -18.3 ;Z Feet
htail_pos_vert = 0.0 ;Y Feet
htail_incidence = 3.2 ;Degrees
htail_sweep = 10.0 ;Degrees, htail leading edge
vtail_area = 18.0 ;Square feet
vtail_span = 4.8 ;Feet, tip to body
vtail_sweep = 40.0 ;Degrees, vtail leading edge
vtail_pos_lon = -16.2 ;Z Feet
vtail_pos_vert = 1.5 ;Y Feet
elevator_area = 16.6 ;Square feet
aileron_area = 18.3 ;Square feet
rudder_area = 6.7 ;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 = 24.0 ;Degrees
elevator_trim_limit = 19.5 ;Degrees
spoiler_limit = 0.0 ;Degrees
spoilerons_available = 0 ;Spoilerons Available?
aileron_to_spoileron_gain = 0 ;Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 ;Degrees
min_flaps_for_spoilerons = 0 ;Min flap handle position
[Flaps.0]
type = 0
[GeneralEngineData]
engine_type = 0
Engine.0 = 0.000, 0.000, 0.000
fuel_flow_scalar = 0.880
min_throttle_limit = 0 ;Minimum percent throttle.
[piston_engine]
power_scalar = 1.0 ;Piston power scalar
cylinder_displacement = 90.0 ;Cubic inches per cylinder
compression_ratio = 8.5
number_of_cylinders = 4
max_rated_rpm = 2700
max_rated_hp = 180
fuel_metering_type = 0 ;0=Fuel Injected
cooling_type = 0 ;0=Air, 1=Liquid
normalized_starter_torque = 0.3 ;Starter torque factor
turbocharged = 0 ;0=FALSE
max_design_mp = 0 ;(inHg)
min_design_mp = 0 ;(inHg)
critical_altitude = 0 ;(feet)
emergency_boost_type = 0 ;0=None
emergency_boost_mp_offset = 0 ;MP from emergency boost
emergency_boost_gain_offset = 0 ;MP multiplier
fuel_air_auto_mixture = 0 ;Automixture available? 0=FALSE
auto_ignition = 0 ;Auto-Ignition available? 0=FALSE
max_rpm_mechanical_efficiency_scalar = 1.0
idle_rpm_mechanical_efficiency_scalar = 1.0
max_rpm_friction_scalar = 1.0
idle_rpm_friction_scalar = 1.0
[propeller]
thrust_scalar = 1.3 ;Propeller thrust scalar
propeller_type = 1 ;1=Fixed Pitch
propeller_diameter = 6.3 ;(feet)
propeller_blades = 2
propeller_moi = 5.0
beta_max = 0
beta_min = 0
min_gov_rpm = 0 ;Miminum governed RPM
prop_tc = 0 ;Prop time-constant
gear_reduction_ratio = 1.0 ;Propeller gear reduction ratio
fixed_pitch_beta = 5 ;Fixed pitch prop angle (degrees)
low_speed_theory_limit = 80 ;(feet/second)
prop_sync_available = 0 ;Prop synchronization 0=FALSE
prop_deice_available = 0 ;Prop de-icing 0=FALSE
prop_feathering_available = 0 ;Prop feather 0=FALSE
prop_auto_feathering_available = 0 ;Prop auto-feather 0=FALSE
min_rpm_for_feather = 0 ;Min RPM for prop feather
beta_feather = 0 ;Feather pitch angle (degrees)
power_absorbed_cf = 0 ;Coefficient of friction
defeathering_accumulators_available = 0 ;Defeather accumulators 0=FALSE
prop_reverse_available = 0 ;0=FALSE
minimum_on_ground_beta = 0 ;Min pitch on ground (degrees)
minimum_reverse_beta = 0 ;Min pitch in reverse (degrees)
[fuel]
Center1 = 0.000, 0.000, 0.000, 200.000, 10.000
fuel_type = 1 ;1=Avgas
number_of_tank_selectors = 1
electric_pump = 1
[electrical]
electric_always_available = 1
[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
[gear_warning_system]
gear_warning_available = 0
[brakes]
parking_brake = 0 ;Parking brake not available
toe_brakes_scale = 0.0 ;Brake scalar
[hydraulic_system]
normal_pressure = 0.0
[direction_indicators]
turn_indicator.0 =3,0 ;3=Electro-Mag Slaved Compass
direction_indicator.0 =1,0
[attitude_indicators]
attitude_indicator.0 = 0 ;0=None
[turn_indicators]
turn_indicator.0 = 0 ;0=None
[stall_warning]
type = 0
[autopilot]
autopilot_available = 1
flight_director_available = 0
default_vertical_speed = 700.0
autothrottle_available = 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 = 1.0
pitch_takeoff_ga = 8.000000
[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
[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
