Newsgroup: it.comp.giochi.simulatori.volo
Titolo: Dinamiche Oliveira per PSS A320

Ho installato le dinamiche di Pedro Oliverira v.10 per il pss e devo
dire che č diventato molto piu' reale e stabile. 
Unico problema, con il load manager mi va in Type Mismatch appena
seleziono l'aereo A320 e non so il perchč. Quindi non riesco a settare
lo ZFW. 
Qualcuno puo' aiutarmi? DI strano non ho fatto nulla in quanto
l'installazione prevde solo la copia dei file cfg e AIR nel folder del
PSS.
 
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il mio load manager funziona, però abitualmente uso quello di 
fspassenger... non so aiutarti, ti consiglierei di reinstallare il 320 
della pss e poi rimettere le dinamiche di Pedro e vedere se poi 
funziona... sicuramente non è una incompatibilità tra pss e dinamiche di 
Pedro perchè conosco altri che usano tranquillamente PSS320 + dinamiche 
"Pedro" e load manager.
ciao,
giancarlo
ciao,
Giancarlo

L'ho già fatto ma non succede nulla, anche perchè appena gli rimetto il
suo aircraft.cfg (pss) funziona tutto perfettamente. Io credo che il
load manager editi il cfg e che per qualche motivo trova qualche
parametro strano!!


valtur ha scritto:

questo è il mio cfg (pedro o.), ciao, giancarlo :
// by Pedro Oliveira
[fltsim.0]
title=Airbus A320-200-CFM56-5B4 - PSS
sim=Airbus320-200-CFM56-5B4
model=cfm
panel=
sound=cfm
texture=alital
kb_checklists=
kb_reference=
atc_id=
atc_airline=
atc_flight_number=
atc_heavy=0
ui_manufacturer=Airbus
ui_type=A320-200-CFM56-5B4 - PSS
ui_variation=
description=Highly accurate FDE for Airbus A320-200 w/ CFM56-5B4 engines.
atc_id_color=0000000000
visual_damage=0
[fltsim.1]
title=Airbus A320-200-IAE - PSS
sim=Airbus320-200-IAE
model=iae
panel=
sound=iae
texture=
kb_checklists=
kb_reference=
atc_id=
atc_airline=
atc_flight_number=
atc_heavy=0
ui_manufacturer=Airbus
ui_type=A320-200-IAE - PSS
ui_variation=
description=Highly accurate FDE for Airbus A320-200 w/ IAE engines.
atc_id_color=0000000000
visual_damage=0
[General]
atc_type=Airbus
atc_model=A320
editable=0
performance=Engines\nrated at 26,500 lbs\n\nTypical Cruise Speed\n0.78 
Mach at 35,000 ft\n\nMax Speed\nVmo 350 kts    Mmo 0.82 
Mach\n\nRange(150 pax)\n2,900 nm (5,374 km)\n\nMax Fuel\n42,230 lbs 
(6,303 US gal)\n\nMax Takeoff Weight\n162,040 lbs\n\nMax Gross Weight 
(taxi weight)\n162,900 lbs\n\nMax Payload\n42,370 lbs
[pitot_static]
vertical_speed_time_constant = 99
[WEIGHT_AND_BALANCE]
max_gross_weight = 162900
empty_weight = 90400
reference_datum_position =  0.0, 0.0, 0.0
empty_weight_CG_position = -1.45, 0.0, 0.0                       // 
(feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170.0,   41.91, -2.0, 1.64, Pilot" 
//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170.0,   41.91,  2.0, 1.64, Co-Pilot" 
//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "11115.0,  18.9,  0.0, 1.64, Front cabin" 
//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "3505.0,  29.17,  0.0, -3.28, Front cargo" 
//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "4000.0, -50.45,  0.0, 3.05, Rear cargo" 
//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "11310.0, -18.49,  0.0, 1.64, Rear cabin" 
//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_roll_MOI    = 4250000
empty_weight_pitch_MOI   = 2250000
empty_weight_yaw_MOI     = 4000000
empty_weight_coupled_MOI = 0
[fuel]
LeftMain =   -0.82,  -6.16, -0.82, 1829.5, 0.0
RightMain =  -0.82,   6.16, -0.82, 1829.5, 0.0
LeftAux =    -4.93, -26.7,   0.82,  232.0, 0.0
RightAux =   -4.93,  26.7,   0.82,  232.0, 0.0
Center1 =     0.0,    0.0,  -4.11, 2180.0, 0.0
fuel_type = 2                        //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump = 0
[airplane_geometry]
wing_area=1317.5
wing_span=111.25
wing_root_chord=17.67
wing_dihedral=4.499
wing_incidence=-0.784
wing_twist=0.0
oswald_efficiency_factor=0.75
wing_winglets_flag=1
wing_sweep=25.0
wing_pos_apex_lon=16.0
wing_pos_apex_vert=0.0
htail_area=337.0
htail_span=41.67
htail_pos_lon=-50.0
htail_pos_vert=0.0
htail_incidence=0.0
htail_sweep=0.0
vtail_area=249.0
vtail_span=17.992
vtail_sweep=0.0
vtail_pos_lon=-35.83
vtail_pos_vert=5.83
elevator_area=70.5
aileron_area=26.8
rudder_area=56.2
elevator_up_limit=28.0
elevator_down_limit=20.0
aileron_up_limit=26.0
aileron_down_limit=26.0
rudder_limit=25.0
elevator_trim_limit=18.5
spoiler_limit=35.0
spoilerons_available=1
aileron_to_spoileron_gain=1.10
min_ailerons_for_spoilerons=11
min_flaps_for_spoilerons=0
[Reference Speeds]
flaps_up_stall_speed     = 128.0
full_flaps_stall_speed   = 102.0
cruise_speed             = 455.0
max_mach                 =   0.82
max_indicated_speed      = 350.0
[Flaps.0]
type=1
span-outboard         = 0.8
extending-time        = 21.0
flaps-position.0      = 0.0
flaps-position.1      = 7.0
flaps-position.2      = 14.0
flaps-position.3      = 21.0
flaps-position.4      = 28.0
flaps-position.5      = 35.0
damaging-speed        = 233.0
blowout-speed         = 250.0
lift_scalar           = 0.85
drag_scalar           = 0.8
pitch_scalar          = 1.1
system_type           = 1                   //Hydraulic
[flaps.1]
type=2                                      // 1 - tail, 2 - lead
span-outboard         = 0.8
extending-time        = 18
flaps-position.0      = 0
flaps-position.1      = 0
flaps-position.2      = 5
flaps-position.3      = 10
flaps-position.4      = 10
flaps-position.5      = 27
damaging-speed        = 260
blowout-speed         = 270
lift_scalar           = 0.4
drag_scalar           = 0.3
pitch_scalar          = 1.2
system_type           = 1                   //Hydraulic
[flight_tuning]
cruise_lift_scalar          = 1.0
parasite_drag_scalar        = 1.0
induced_drag_scalar         = 1.0
elevator_effectiveness      = 1.0
aileron_effectiveness       = 1.0
rudder_effectiveness        = 1.15
pitch_stability             = 1.0
roll_stability              = 1.0
yaw_stability               = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0
[GeneralEngineData]
engine_type = 1                             //0=Piston, 1=Jet, 2=None, 
3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 6.98, -12.85, -1.85              //(feet) longitudinal, 
lateral, vertical distance from reference datum
Engine.1 = 6.98,  12.85, -1.85              //(feet) longitudinal, 
lateral, vertical distance from reference datum
fuel_flow_scalar = 1.055                    //Scalar for fuel flow 
efficiency
min_throttle_limit = -0.278;                //Minimum throttle. 
Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain         = 0.002
inlet_area             = 29.0
rated_N2_rpm           = 29920
static_thrust          = 26500
afterburner_available  = 0
reverser_available     = 1
[jet_engine]
thrust_scalar=1.0
[autopilot]
autopilot_available                  = 1.0
flight_director_available            = 1.0
default_vertical_speed               = 1800.0
autothrottle_available               = 1.0
autothrottle_arming_required         = 1.0
autothrottle_takeoff_ga              = 1.0
autothrottle_max_rpm                 = 90.0
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                             = 22.0
max_bank_acceleration                = 1.5
max_bank_velocity                    = 2.5
max_throttle_rate                    = 0.1
nav_proportional_control             = 9.0
nav_integrator_control               = 0.25
nav_derivative_control               = 0.0
nav_integrator_boundary              = 2.5
nav_derivative_boundary              = 0.0
gs_proportional_control              = 9.52
gs_integrator_control                = 0.26
gs_derivative_control                = 0.0
gs_integrator_boundary               = 0.7
gs_derivative_boundary               = 0.0
yaw_damper_gain                      = 1.0
[contact_points]
         //0  Class                        <0=none,1=wheel, 2=scrape, 
3=float>
         //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 = 1,  33.85,   0.0,   -12.0,   1574.8,   0.0, 1.68, 75.0, 0.41, 
2.5, 0.65,   9.0,  9.4, 0.0, 0.0, 0.0
point.1 = 1,  -3.80, -12.417, -12.3,   1574.803, 1.0, 1.68,  0.0, 1.0, 
2.5, 0.52,  13.0, 11.7, 2.0, 0.0, 0.0
point.2 = 1,  -3.80,  12.417, -12.3,   1574.803, 2.0, 1.68,  0.0, 1.0, 
2.5, 0.52,  13.1, 11.9, 3.0, 0.0, 0.0
point.3 = 2, -13.75, -54.58,   -0.5,    750.925, 0.0, 0.0,   0.0, 0.0, 
0.0, 0.0,    0.0,  0.0, 5.0, 0.0, 0.0
point.4 = 2, -13.75,  54.58,   -0.5,    750.925, 0.0, 0.0,   0.0, 0.0, 
0.0, 0.0,    0.0,  0.0, 6.0, 0.0, 0.0
point.5 = 2, -71.25,   0.0,     0.75,   750.925, 0.0, 0.0,   0.0, 0.0, 
0.0, 0.0,    0.0,  0.0, 9.0, 0.0, 0.0
point.6 = 2,  51.67,   0.0,    -8.17,   750.925, 0.0, 0.0,   0.0, 0.0, 
0.0, 0.0,    0.0,  0.0, 4.0, 0.0, 0.0
point.7 = 5, -50.9,  -19.25,  -19.3,   1600,     0.0, 0.0,  70.0, 0.0, 
0.0, 5.0,    3.0,  3.2, 0.0, 0.0, 0.0
point.8 = 5, -50.9,   19.25,  -19.3,   1600,     0.0, 0.0,  70.0, 0.0,
static_pitch=0
static_cg_height=10.9
gear_system_type=1      //Hydraulic
[gear_warning_system]
gear_warning_available = 0    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  5.0     //Flap angle that activates warning at idle
flap_limit_power   = 25.5     //Flap angle that activates warning at 
above idle
[brakes]
toe_brakes_scale=0.73
parking_brake=1
[hydraulic_system]
normal_pressure=3000.0    //PSI
electric_pumps=0          //no electric pumps
engine_map=1,1,0,0        //pumps on Eng1,2
[Views]
eyepoint=50.852, -1.7487, 4.229              ; Longitude, Latitude and 
Vertical position from Reference Point, (FEET)
[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, 0, 17.0
avionics=1, 0 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 0, 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, 0 , 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, 0 , 17.0
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=5,   17.0,   0.0, -9.0,  PSS_Light , // main land
light.1=3,  -50.0,    4.0, 20.0, PSS_logo , // logo
light.2=3,  -50.0,   -4.0, 20.0, PSS_logo , // logo
light.3=5,   52.0,    0.0, -6.0, PSS_Light , // Nose light
light.4=3,  -4.0, -53.44,  3.33, nav_red.fx ,
light.5=3,  -4.0,  53.44,  3.33, nav_green.fx ,
light.6=3, -61.2,  0.00,  4.0, nav_white.fx ,
light.7=2,  -4.3, -53.90,  3.34, PSS_strobe_Airbus ,
light.8=2,  -4.3,  53.90,  3.34, PSS_strobe_Airbus ,
light.9=1,   25.28, 0.00, -5.00, pss_beacon ,
light.10=1,   27.0, 0.00,  8.60, pss_beacon ,
light.11=4,   52.0,  0.00,  4.5,  PSS_vclight ,
light.12=2,  -61.2, 0.00,  4.0, PSS_strobe_Airbus ,
[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 = 2
attitude_indicator.1 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[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 = 150, 250
aileron  = 150, 250
rudder   = 150, 250
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[exits]
number_of_exits = 2
exit_rate.0 = 0.4                       ;Percent per second
exit_rate.1 = 0.4                       ;Percent per second
[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

Grazie mille ... ora provo!!!


Ho visto che hai le texture ALitalia.... da dove le hai scaricate? Io
ho trovato solo quelle per A319!!!


valtur ha scritto:

mi pare di averle acquistate sul sito pss... se non ricordo male...
ciao,
giancarlo

Ieri ho fatto un atterraggio con il 320 PSS con dinamiche oliveira,
avevo 20 nodi di vento al traverso e l'aereo si è scostato
completamente dall'ILS e non riusciva a mantenere il localizzatore,
alla fine ho dovuto disconnettere l'AP e andare a mano. Visto che
questo nel 320 vero non succede e tantomeno con il 737 PMDG devo
dedurre che purtroppo (perchè mi piace tanto) il 320 PSS ha ancora
qualche buco di volo!!
