Project Airbus Merge für PSS

[Floopy]

Hallo ich suche ein Merge für Project Airbus, bei AVSIM gabs nichts...

 

vllt gibs auch keints :confused: ich weiß es nicht, vllt ihr:(

 

 

Ein anderes Problem ist, der Sound in meinem Cockpit geht nach paar Sekunden aus. Das gleiche Sound Set hab ich für meinen IFDG Airbus auch benutzt, und dort bleibt der Cockpit sound...vllt wisst ihr mehr drüber:(

[Timm Rehberg]

Hi,

 

ich bin mir soooooooo sicher dass du z.B. als erste Anlaufstelle im Project-Airbus Forum (http://www.pairbus.com/) etwas dazu finden wirst.

 

Wenn nicht dort, dann suche mal bei Google nach "Project Airbus PSS Merge"

 

 

Grüße!:005:

[D-EBIP]

Moin Christian,

 

disch kann jeholfen werde:

 

http://www.pairbus.com/board/viewtopic.php?p=1109#p1109

 

Viel Spaß mit dem Bus! :)

[Floopy]

^^ *grins* danke jungs;)

[Patrick C.]

Hallo zusammen

 

Vielleicht könnt Ihr mir auch weiterhelfen ich krieg das Merge einfach nicht mehr richtig hin, seit ich den FS neu installiert habe.

Das Flugverhalten stimmt meiner Meinung überhaupt nicht und im Anflug ist es extrem schwierig an Geschwindigkeit zu verlieren.

 

Ich habe zuerst den PA ModelOrdner in den PSSordner gepakt und alles in von der PSS Aircraft.cfg übernommen ausser lights, flaps und contact Points.

 

Wie habt Ihr den PA gemergt und welche Air Datei verwendet Ihr?

Gruss

Patrick

[CitationCJ]

Henning hat ja oben einen Link gepostet:

 

http://www.pairbus.com/board/viewtopic.php?p=1109#p1109

 

 

Einfach das machen, was Demetris dort schreibt ( habe den Vogel seit dem Merge noch nicht geflogen ).

[Patrick C.]

Henning hat ja oben einen Link gepostet:

 

http://www.pairbus.com/board/viewtopic.php?p=1109#p1109

 

 

Einfach das machen, was Demetris dort schreibt ( habe den Vogel seit dem Merge noch nicht geflogen ).

 

Das hat mir leider nicht weitergeholfen. Ich habe einfach extrem schlechte Flugeigenschaften. Teilweise kriege ich den Bus fast nicht hoch, im Anflug flieg er immer in einem Anstellwinkel von +10°, das sind alles "Probleme", welche ich früher nicht hatte. Die air.Datei habe ich von PSS320C.

Ich hänge hier mal meine Aircraft.cfg an, findet evtl. jemand einen Fehler?

Besten Dank und Gruss

Patrick

 

[fltsim.0]

title=PSS A320 CFM Edelweiss

ui_variation=PSS A320 CFM Edelweiss

sim=A320c

ui_type=A320c

sound=CFM

model=CFM

texture=edelwi

atc_airline=World

panel=

checklists=

atc_id=AB320

atc_flight_number=PS320

atc_heavy=0

ui_manufacturer=Airbus

visual_damage=1

description=Designed to compete with the Boeing 737 and McDonnell Douglas MD-80, The A319/320/321 were Airbus' first entry in the narrow-body market. Although the aircraft borrows some features from the larger A300 and A310, it is essentially a new design equipped with many state-of-the-art engineering innovations. For example, The A319/320/321 were the first commercial jetliners with a full fly-by-wire control system. Other advanced features include widespread use of composite materials to reduce weight, sophisticated avionics including a gust-alleviation system allowing a smoother ride, advanced cockpit warning systems, and high-technology engines to reduce noise and fuel consumption. COPYRIGHT 2002 PHOENIX SIMULATION SOFTWARE

 

[fltsim.1]

title=PSS A320 Swiss International Airlines

ui_variation=PSS A320 Swiss

sim=A320c

ui_type=A320-211

sound=cfm

model=pa

texture=lx

atc_airline=Swiss

panel=

checklists=

atc_id=HB-IJS

atc_flight_number=1839

atc_heavy=0

ui_manufacturer=Airbus

visual_damage=1

description=Designed to compete with the Boeing 737 and McDonnell Douglas MD-80, The A319/320/321 were Airbus' first entry in the narrow-body market. Although the aircraft borrows some features from the larger A300 and A310, it is essentially a new design equipped with many state-of-the-art engineering innovations. For example, The A319/320/321 were the first commercial jetliners with a full fly-by-wire control system. Other advanced features include widespread use of composite materials to reduce weight, sophisticated avionics including a gust-alleviation system allowing a smoother ride, advanced cockpit warning systems, and high-technology engines to reduce noise and fuel consumption. COPYRIGHT 2002 PHOENIX SIMULATION SOFTWARE

 

[fltsim.2]

title=PSS A320 Swiss EM08 International Airlines

ui_variation=PSS A320 Swiss EM2008

sim=A320c

ui_type=A320-211

sound=cfm

model=pa

texture=lx08

atc_airline=Swiss

panel=

checklists=

atc_id=HB-IJM

atc_flight_number=1839

atc_heavy=0

ui_manufacturer=Airbus

visual_damage=1

description=Designed to compete with the Boeing 737 and McDonnell Douglas MD-80, The A319/320/321 were Airbus' first entry in the narrow-body market. Although the aircraft borrows some features from the larger A300 and A310, it is essentially a new design equipped with many state-of-the-art engineering innovations. For example, The A319/320/321 were the first commercial jetliners with a full fly-by-wire control system. Other advanced features include widespread use of composite materials to reduce weight, sophisticated avionics including a gust-alleviation system allowing a smoother ride, advanced cockpit warning systems, and high-technology engines to reduce noise and fuel consumption. COPYRIGHT 2002 PHOENIX SIMULATION SOFTWARE

 

[fltsim.3]

title=PSS A320 Tunisair

ui_variation=PSS A320 Tunisair

sim=A320c

ui_type=A320-211

sound=cfm

model=pa

texture=tunisair

atc_airline=Tunair

panel=

checklists=

atc_id=TS-

atc_flight_number=1839

atc_heavy=0

ui_manufacturer=Airbus

visual_damage=1

description=Designed to compete with the Boeing 737 and McDonnell Douglas MD-80, The A319/320/321 were Airbus' first entry in the narrow-body market. Although the aircraft borrows some features from the larger A300 and A310, it is essentially a new design equipped with many state-of-the-art engineering innovations. For example, The A319/320/321 were the first commercial jetliners with a full fly-by-wire control system. Other advanced features include widespread use of composite materials to reduce weight, sophisticated avionics including a gust-alleviation system allowing a smoother ride, advanced cockpit warning systems, and high-technology engines to reduce noise and fuel consumption. COPYRIGHT 2002 PHOENIX SIMULATION SOFTWARE

 

 

[exits]

number_of_exits=2

exit_rate.0=0.25

exit_rate.1=0.25

 

[Views]

eyepoint=50.852, -1.7487, 4.229

 

[lights]

Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.4=3, -13.90, -55.25, 2.45, pss_navred.fx ,

light.5=3, -13.90, 55.25, 2.45, pss_navgre.fx ,

light.6=3, -69.70, 0.00, 4.70 , pss_navwhi.fx ,

light.7=2, -69.70, 0.00, 4.70, PSS_strobe_Airbus ,

light.8=2, -13.95, -55.25, 2.45, PSS_strobe_Airbus ,

light.9=1, 6.8, 0.00, -5.80, pss_beacon ,

light.10=1, 3.83, 0.00, 8.47, pss_beacon ,

light.11=4, 44.41, 0.00, 3.50, PSS_vclight ,

light.12=2, -13.95, 55.25, 2.45, PSS_strobe_Airbus ,

[General]

atc_type=AIRBUS

atc_model=A320

performance=Dimensions: Wing span: 111 ft 3 in (33.91 m) \n Length: 123 ft 3 in (37.57 m) \n Height: 38 ft 9.50 in (11.80 m) \n Weights: \n Empty: 91,675 lb (41,583 kg) \n Max take-off: 169,765 lb (77,000 kg) \n Performance: Cruise speed: 608 mph (978.48 km/h) \n Max Operating altitude: 40,000 ft (12,192 m) \n Maximum range: 3,222 miles (5,185 km) \n Powerplants: Two IAE V2525-A5 rated at 25,000 lb (111.2 kN) or Two CFM International CFM56-5B4 rated at 26,500 lb (117.9 kN). Hi-bypass Turbofans

 

 

[pitot_static]

vertical_speed_time_constant=99

 

[GROUND_REACTION]

MAX_STEERING_ANGLE=75

 

[GeneralEngineData]

engine_type=1

Engine.0=3.333333,-17.500000,-2.500000

Engine.1=3.333333,17.500000,-2.500000

fuel_flow_scalar=1.250000

min_throttle_limit=-0.499939

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[direction_indicators]

direction_indicator.0=3,0

 

[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

 

[Flaps.0]

type=1

span-outboard=0.85

extending-time=21.000

system_type=1

damaging-speed=233.000

blowout-speed=250.000

flaps-position.0=0.000,

flaps-position.1=7.000, //0 in real life

flaps-position.2=14.000, //10

flaps-position.3=21.000, //14

flaps-position.4=28.000, //21

flaps-position.5=35.000, //25

lift_scalar=0.0

drag_scalar=0.0

 

 

[flaps.1]

type=2 // slats

span-outboard=0.95 // 0.0 .. 1.0

extending-time=9 // seconds

flaps-position.0=0

flaps-position.1=18,

flaps-position.2=18,

flaps-position.3=22,

flaps-position.4=22,

flaps-position.5=27,

blowout-speed=260 // KIAS

lift_scalar=0.35

drag_scalar=0.25

pitch_scalar=0.3

system_type=1

 

[flaps.2] //ailerons

type=2

span-outboard=0.85

extending-time=11.000

system_type=1

damaging-speed=233.000

blowout-speed=250.000

flaps-position.0=0.000,

flaps-position.1=0.000,

flaps-position.2=5.000,

flaps-position.3=5.000,

flaps-position.4=5.000,

flaps-position.5=5.000,

lift_scalar=0.25

drag_scalar=0.30

 

[flaps.3] //actual flaps

type=1

span-outboard=0.85

extending-time=21.000

system_type=1

damaging-speed=233.000

blowout-speed=250.000

flaps-position.0=0.000,

flaps-position.1=0.000,

flaps-position.2=10.000,

flaps-position.3=15.000,

flaps-position.4=20.000,

flaps-position.5=35.000,

lift_scalar=0.80 //1.178

drag_scalar=1.01

 

[WEIGHT_AND_BALANCE]

reference_datum_position=0.000000,0.000000,0.000000

max_number_of_stations=50

 

station_load.0 = 0450, 0.0, 0.0, 0.0 //Weight Crew (lbs) LEAVE

station_load.1 = 3000, 0.0, 0.0, 0.0 //Weight Galleys (lbs) LEAVE

station_load.2 = 5670, 0.0, 0.0, 0.0 //Weight Baggage (lbs) Baggage

station_load.3 = 9280, 0.0, 0.0, 0.0 //Weight Cargo (lbs) Cargo

station_load.4 = 3420, 0.0, 0.0, 0.0 //Weight Psgr Sect OA (lbs) First

station_load.5 = 18360, 0.0, 0.0, 0.0 //Weight Psgr Sect OB (lbs) Coach

 

empty_weight= 90400

empty_weight_roll_MOI=3900000.000000

empty_weight_pitch_MOI=3000000.000000

empty_weight_yaw_MOI=3000000.000000

empty_weight_coupled_MOI=250.000000

empty_weight_CG_position=0.000000,0.000000,0.000000

max_gross_weight=215775.000000

 

*************************************************

 

 

 

[fuel]

Center1=-2.000000,0.000000,0.000000,2174.000000,0.000000

LeftMain=-3.000000,-19.000000,0.000000,2060.000000,0.000000

RightMain=-3.000000,19.000000,0.000000,2060.000000,0.000000

fuel_type=2.000000

number_of_tank_selectors=1

electric_pump=1

[airplane_geometry]

wing_area=1317.000000

wing_span=111.166667

wing_root_chord=12.000000

wing_dihedral=6.289673

wing_incidence=1.499634

wing_twist=-0.812988

oswald_efficiency_factor=0.696989 //was 0.4

wing_winglets_flag=1

wing_sweep=0.000000

wing_pos_apex_lon=13.600000

wing_pos_apex_vert=0.000000

htail_area=328.000000

htail_span=40.000000

htail_pos_lon=-50.000000

htail_pos_vert=0.000000

htail_incidence=2.993774

htail_sweep=0.000000

vtail_area=249.000000

vtail_span=17.991665

vtail_sweep=0.000000

vtail_pos_lon=-50.000000

vtail_pos_vert=20.500000

elevator_area=70.500000

aileron_area=26.800000

rudder_area=56.200000

elevator_up_limit=30 //was 14

elevator_down_limit=30

aileron_up_limit=30.000070

aileron_down_limit=30.000070

rudder_limit=30.000070

elevator_trim_limit=30 //was 20

spoiler_limit=59.988681

spoilerons_available=1

aileron_to_spoileron_gain=3.000000

min_ailerons_for_spoilerons=9.969466

min_flaps_for_spoilerons=0.000000

[contact_points]

static_pitch=-0.319722

static_cg_height=11.60811023622

 

point.0=1.0, 38.84,0.0,-11.9619,800,0.0,1.53379,68.0,1.0,1.4390,0.680000, 13.2,12.9,0.000000,252.000000,282.0

point.1=1.0,-3.660,-12.458,-12.22,1200,1.000000,1.680382,0.000000,0.72,1.5419948,0.81,14.000000,13.700000,2.000000,252.000000,282.000000

point.2=1.0,-3.660,12.458,-12.22,1200,2.000000,1.680382,0.000000,0.72,1.5419948,0.80,14.200000,13.300000,2.000000,252.000000,282.000000

point.3=2.0,-13.750000,-54.583333,-0.500000,750.924659,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000

point.4=2.0,-13.750000,54.583333,-0.500000,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0

point.5=2.0,-71.250000,0.0,0.750,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0

point.6=2.0,51.666667,0.0,-8.166667,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0

gear_system_type=0

[TurbineEngineData]

fuel_flow_gain=0.002000

inlet_area=22.000000

rated_N2_rpm=29920.000000

static_thrust=25000.000000

afterburner_available=0

reverser_available=1

[Reference Speeds]

flaps_up_stall_speed=190.000000

full_flaps_stall_speed=152.000000

cruise_speed=552.421072

max_indicated_speed=350.000000

max_mach=0.821240

[keyboard_response]

elevator=150.000000,250.000000

aileron=150.000000,250.000000

rudder=150.000000,250.000000

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

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=1.000000

[brakes]

toe_brakes_scale=0.676592

parking_brake=1

[gear_warning_system]

gear_warning_available=0

pct_throttle_limit=0.099976

flap_limit_power=25.496622

flap_limit_idle=5.042029

[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

[TailHook]

tailhook_length=4

tailhook_position=-15.0, 0.0, -1.0

cable_force_adjust=0.9