;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