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ME 109 Control


Rnglgdj

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I have a lot of ME 109 planes and cannot keep them on the runway at takeoff. They all seem to drift to the left no matter how much right rudder I give to max.

 

What do I adjust in the cfg to increase the rudder deflection.

 

Thanks

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In the [flight_tuning] section, change:

rudder_effectiveness =1.0

to:

rudder_effectiveness =1.5

These figures are percentages, so changing 1.0 to 1.5 increases rudder effectiveness by 50%.

If you find that's too much, reduce it to 1.25. If it's not enough, increase to 1.75 and so on. You can fine tune it by .01 at a time to get it spot on.

Tim Wright "The older I get, the better I was..."

Xbox Series X, Asus Prime H510M-K, Intel Core i5-11400F 4.40GHz, 16Gb DDR4 3200, 2TB WD Black NVME SSD, 1TB Samsung SATA SSD

NVidia RTX3060 Ti 8Gb, Logitech Flight Yoke System, CH Pro Pedals, Acer K272HL 27", Windows 11 Home x64

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I have a lot of ME 109 planes and cannot keep them on the runway at takeoff. They all seem to drift to the left no matter how much right rudder I give to max.

 

What do I adjust in the cfg to increase the rudder deflection.

 

Thanks

 

It can also help if you open the throttle slowly after letting the brakes off.

Keith

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Messerschmitt BF 109E7 for FS 2004 for one of them

 

Sorry, not helpful! Payware?? That's all I can find with that description.

 

I did find a freeware BF-109E_7 to try!

Edited by mrzippy

Still thinking about a new flightsim only computer!  ✈️

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I have a lot of ME 109 planes and cannot keep them on the runway at takeoff. They all seem to drift to the left no matter how much right rudder I give to max.

 

What do I adjust in the cfg to increase the rudder deflection.

 

Thanks

 

Nothing, Instead hold the tail down with aft stick until the rudder comes `alive`. The Messerschmitt was known for the narrow-track undercarriage and canted wheels, making it susceptible to swinging on take-off and landing. Holding the tail down puts the tailwheel in firm contact, and lessens reliance on the ineffective rudder.

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No not payware it is in the FS library Messerschmitt_Bf109E7 I had to change the rudder eff to 1.75 to get some correction Has anyone mastered the 109 on take off and what file????

 

OK, it is the same one I found on another site. Are you in the cockpit or outside view when taking off?

 

I found that there is good rudder steering while taxiing at low speed with rudder movement full left to right. Takeoff is difficult when in the cockpit until the tail lifts and visibility of the runway occurs. I did notice that there is NO rudder movement after liftoff until the wheels touch the deck again.

 

Since it is a 2D cockpit only, maybe hitting the w key to give the open view during takeoff might help.

Still thinking about a new flightsim only computer!  ✈️

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I just tried another test flight. I did find that I had "autorudder" checked in the settings so I disabled that and now have full rudder control in the air. I used the mini panel while doing the takeoff and there is pull to the left, but very correctable using the rudder and I managed to stay on the runway for takeoff.

 

I have sliders maxed out to the right for all of the realism settings, P-factor, etc. I don't see any way to dramatically change it so it travels in a straight line during takeoff.

Edited by mrzippy

Still thinking about a new flightsim only computer!  ✈️

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Hi Sir,

Sorry I can NOT confirm your analysis for ANY of the BF-109!! from Mr. Scrub.

 

I use the planes from MR. Scrub.

 

Do you refer to the following ZIP file ??

 

"messerschmitt_bf109e7.zip"

 

IF yes, than can you send me YOUR aircraft.CFG file ??

 

I will fix it for you, Sir.

 

EVEN at 150 KIAS on T.O. the plane tracks down the RWY "DEAD CENTER" NOT even using the Joystick.

 

Absolutely NO diversion in EITHER direction.

 

I would send you my CFG IF I would know your email address.

 

My is: gkcherry1@t-online.de

 

Sincerely

G. Kirschstein

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[fltsim.0]

title=BF109E_III/JG26

sim=BF109E7

model=

panel=

sound=

texture=

checklists=

description=Bf-109 E-3 III/JG26 Adolf Galland "Black 1", France 1940

ui_manufacturer=Messerschmitt-A

ui_type=ME109E Emil

ui_variation=JG/26

atc_id_color=0000000000

visual_damage=0

 

[fltsim.1]

title=BF109E JG27 Libya

sim=BF109E7

model=trop

panel=

sound=

texture=Steinhausen

checklists=

description=Bf 109E-7/B, flown by Unteroffizier Steinhausen . Günther Steinhausen was credited with 40 victories over North Africa.

ui_manufacturer=Messerschmitt-A

ui_type=ME109E Emil

ui_variation=Trop JG27 Libya

atc_id_color=0000000000

visual_damage=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=6000 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; 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=3250 ; 0 - 10000

ground_bumps_angle1=8900 ; 0 - 35999 degrees

ground_bumps_intercept1=5.0

ground_bumps_slope1=0.48

ground_bumps_magnitude2=750 ; 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

 

[flight_tuning]

elevator_effectiveness=1.0

aileron_effectiveness=1.0

rudder_effectiveness=3.75

elevator_trim_effectiveness=3.0

pitch_stability=1.1

roll_stability=1.0

yaw_stability=1.0

cruise_lift_scalar=1.0

parasite_drag_scalar=1.0

induced_drag_scalar=1.0

 

[weight_and_balance]

empty_weight=4419

empty_weight_CG_position=0.085,0,0

max_number_of_stations=50

;basic weight: Second CoG for guns and protection (adds to empty weight)

station_load.0=633,0,0,0

;pilot weight and personal equipment

station_load.1=200,-2,0,0.8

reference_datum_position=0.000000,0.000000,0.000000

empty_weight_roll_MOI=6870.000000

empty_weight_pitch_MOI=7920.000000

empty_weight_yaw_MOI=11203.000000

empty_weight_coupled_MOI=0.000000

max_gross_weight=7878.000000

 

[piston_engine]

 

power_scalar=1.0

cylinder_displacement=175.540000

compression_ratio=6.800000

number_of_cylinders=12

max_rated_rpm=2700.000000

max_rated_hp=1175.000000

fuel_metering_type=0

cooling_type=1

normalized_starter_torque=0.035000

turbocharged=1

max_design_mp=39.999999

min_design_mp=9.000000

critical_altitude=33822.000000

emergency_boost_type=0

emergency_boost_mp_offset=2.680000

emergency_boost_gain_offset=0.540000

fuel_air_auto_mixture=1

auto_ignition=0

max_rpm_mechanical_efficiency_scalar=1.000000

idle_rpm_mechanical_efficiency_scalar=1.000000

max_rpm_friction_scalar=1.000000

idle_rpm_friction_scalar=1.000000

 

[propeller]

 

thrust_scalar=1.0

propeller_type=0

propeller_diameter=10.166700

propeller_blades=4

propeller_moi=32.800000

beta_max=65.000000

beta_min=15.000000

min_gov_rpm=400.000000

prop_tc=0.010000

gear_reduction_ratio=1.684000

fixed_pitch_beta=0.000000

low_speed_theory_limit=80.000000

prop_sync_available=0

prop_deice_available=0

prop_feathering_available=1

prop_auto_feathering_available=0

min_rpm_for_feather=70.000000

beta_feather=88.500000

power_absorbed_cf=0.900000

defeathering_accumulators_available=0

prop_reverse_available=0.000000

minimum_on_ground_beta=0.000000

minimum_reverse_beta=0.000000

 

[ground_reaction]

main_gear_static_compression=0.3

center_gear_static_compression=0.33

main_gear_damping_ratio=0.9

center_gear_damping_ratio=0.8

 

[electrical]

max_battery_voltage = 24.0

generator_alternator_voltage = 28.0

max_generator_alternator_amps = 60.0

 

[folding_wings]

wing_fold_system_type = 1 ;0=None

fold_rates = 1.0,1.0 ;Percent per second

 

[contact_points]

 

//0 Class

//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,-16.67,0,-1.80,2165.3544,0,0.534815,45,0.5,3,0.80,0,0,0,0,0

point.1=1,2.83,-3.16,-6.30,2165.3544,1,1.35,0,0.5,3,0.8,3.5,9,2,128,143

point.2=1,2.83,3.16,-6.30,2165.3544,2,1.35,0,0.5,3,0.8,4.5,6.5,3,128,143

point.3=2,0,-16.583,0.833,1181.102,0,0,0,0,0,0,0,0,5,0,0

point.4=2,0,16.583,0.833,1181.102,0,0,0,0,0,0,0,0,6,0,0

point.5=2,-19.75,0,1.833,1181.102,0,0,0,0,0,0,0,0,9,0,0

point.6=2,7.416,0,-3.75,1181.102,0,0,0,0,0,0,0,0,4,0,0

point.7=2,0,-16.583,-0.166,0,0,0,0,0,0,0,0,0,7,0,0

point.8=5,7.14,0,-0.5,1600,0,0,10,0.4,2.5,1,0.2,0.2,4

 

static_pitch=13.18

static_cg_height=4.850

gear_system_type=1

 

[flaps.0]

type=1 // 1 - tail, 2 - lead

span-outboard=0.4 // 0.0 .. 1.0

extending-time=5 // seconds

flaps-position.0=0 // degrees, KIAS

flaps-position.1=15,193 // degrees, KIAS

flaps-position.2=25,165 // degrees, KIAS

flaps-position.3=33,137 // degrees, KIAS

flaps-position.4=45,109 // degrees, KIAS

damaging-speed=177 // KIAS

blowout-speed=214 // KIAS

 

 

[Views]

eyepoint=-2.5, 0.0, 2.00

 

 

[General]

performance=Length: 8.74 m, 26 64'\nWing span: 9.86 m, 32 35'\nWeight: 4817lbs empty, 6834lbs loaded\nPower: Daimler Benz DB 601A 1175 HP\nWeapons: 2x 7,92mm guns, 3x 20mm cannon\nGMAX mdl by A.F.Scrub January 2013

Category=airplane

[fuel]

Center1=-0.800000,0.000000,-1.000000,105.400000,0.400000

External1=2.300000,0.000000,-4.400000,79.155673,0.155673

fuel_type=1.000000

number_of_tank_selectors=1

electric_pump=0

[airplane_geometry]

wing_area=198.000000

wing_span=32.000000

wing_root_chord=5.750000

wing_dihedral=6.998291

wing_incidence=0.999756

wing_twist=-0.543823

oswald_efficiency_factor=1.066250

wing_winglets_flag=0

wing_sweep=0.000000

wing_pos_apex_lon=0.000000

wing_pos_apex_vert=0.000000

htail_area=28.000000

htail_span=10.000000

htail_pos_lon=-15.250000

htail_pos_vert=0.000000

htail_incidence=0.000000

htail_sweep=0.000000

vtail_area=25.000000

vtail_span=5.700877

vtail_sweep=0.000000

vtail_pos_lon=-16.666667

vtail_pos_vert=2.750000

elevator_area=19.000000

aileron_area=19.000000

rudder_area=19.000000

elevator_up_limit=28.000447

elevator_down_limit=28.000447

aileron_up_limit=16.993928

aileron_down_limit=16.867877

rudder_limit=29.994341

elevator_trim_limit=14.323945

spoiler_limit=16.329297

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=0.300000

positive_g_limit_flaps_up=8.500000

positive_g_limit_flaps_down=7.000000

negative_g_limit_flaps_up=-5.500000

negative_g_limit_flaps_down=-4.600427

[brakes]

toe_brakes_scale=0.598163

parking_brake=1

[gear_warning_system]

gear_warning_available=1

pct_throttle_limit=0.244141

flap_limit_power=40.107046

flap_limit_idle=26.356059

[GeneralEngineData]

engine_type=0

Engine.0=7.500000,0.000000,0.000000

fuel_flow_scalar=1.000000

min_throttle_limit=0.000000

[Reference Speeds]

flaps_up_stall_speed=88.000000

full_flaps_stall_speed=70.400000

cruise_speed=180.936342

max_indicated_speed=406.375000

[keyboard_response]

elevator=303.000000,470.000000

aileron=400.000000,700.000000

rudder=180.000000,260.000000

[autopilot]

autopilot_available=1

flight_director_available=0

default_vertical_speed=700.000000

autothrottle_available=1

autothrottle_arming_required=0

autothrottle_takeoff_ga=0

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=0.000000

[hydraulic_system]

electric_pumps=0

engine_map=1,0,0,0

normal_pressure=6.930556

[stall_warning]

type=1

stick_shaker=1

[attitude_indicators]

attitude_indicator.0=1

[turn_indicators]

turn_indicator.0=1,0

[direction_indicators]

direction_indicator.0=1,0

[pitot_static]

pitot_heat=1.000000

[vacuum_system]

max_pressure=5.000000

vacuum_type=1

electric_backup_pressure=0.000000

engine_map=1,1,1,1

[pneumatic_system]

max_pressure=0.000000

bleed_air_scalar=0.000000

[deice_system]

structural_deice_type=0

 

[sMOKESYSTEM]

smoke.0= -10.00, 0.00, -0.5, fx_su_vaportrail.fx //reference datum vertical, longitudinal, lateral

 

[EFFECTS]

wake = fx_wake

water = fx_spray

dirt = fx_tchdrt

concrete = fx_sparks

touchdown = fx_tchdwn, 1

startup=fx_engstrt

 

[LIGHTS]

//1 Longitudinal - minus rear (feet)

//2 Lateral - minus left (feet)

//3 elevation - minus lower (feet)

 

//#1=beacon #2=strobe #3=nav #10=reheat

//#4=cockpit #5=landing #6=taxi

//#7=recog #8=wing #9=logo

//---------------originals----------------------------

light.0=4, 0.80, -16.00, -0.20, fx_navred

light.1=4, 0.80, 16.00, -0.20, fx_navgre

light.2=4, -4.56, 0.00, -1.20, fx_beacon

light.3=4, -20.15, 0.00, 1.40, fx_strobeh

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[fltsim.0]

title=BF109E_III/JG26

sim=BF109E7

model=

panel=

sound=

texture=

checklists=

description=Bf-109 E-3 III/JG26 Adolf Galland "Black 1", France 1940

ui_manufacturer=Messerschmitt

ui_type=ME109E Emil

ui_variation=JG/26

atc_id_color=0000000000

visual_damage=0

 

[fltsim.1]

title=BF109E JG27 Libya

sim=BF109E7

model=trop

panel=

sound=

texture=Steinhausen

checklists=

description=Bf 109E-7/B, flown by Unteroffizier Steinhausen . Günther Steinhausen was

 

credited with 40 victories over North Africa.

ui_manufacturer=Messerschmitt

ui_type=ME109E Emil

ui_variation=Trop JG27 Libya

atc_id_color=0000000000

visual_damage=0

 

[General]

performance=Length: 8.74 m, 26 64'\nWing span: 9.86 m, 32 35'\nWeight: 4817lbs empty,

 

6834lbs loaded\nPower: Daimler Benz DB 601A 1175 HP\nWeapons: 2x 7,92mm guns, 3x 20mm

 

cannon\nGMAX mdl by A.F.Scrub January 2013

Category=airplane

 

 

 

[flight_tuning]

elevator_effectiveness=1.0

aileron_effectiveness=1.0

rudder_effectiveness=1.0

elevator_trim_effectiveness=1.0

pitch_stability=1.1

roll_stability=1.0

yaw_stability=1.0

cruise_lift_scalar=1.0

parasite_drag_scalar=1.0

induced_drag_scalar=1.0

 

[weight_and_balance]

 

empty_weight_CG_position=0.085,0,0

max_number_of_stations=5

;basic weight: Second CoG for guns and protection (adds to empty weight)

 

station_load.0=633,0,0,0

 

;pilot weight and personal equipment

station_load.1=200,-2,0,0.8

 

reference_datum_position=0.0,0.0,0.0

 

empty_weight_roll_MOI=6870

empty_weight_pitch_MOI=7920

empty_weight_yaw_MOI=11203

empty_weight_coupled_MOI=0

 

empty_weight=4419

max_gross_weight=7878

 

[piston_engine]

 

power_scalar=1.0

cylinder_displacement=175.54

compression_ratio=6.8

number_of_cylinders=12

max_rated_rpm=2700

max_rated_hp=1175

fuel_metering_type=0

cooling_type=1

normalized_starter_torque=0.035

turbocharged=1

max_design_mp=39.9

min_design_mp=9.0

critical_altitude=33822

emergency_boost_type=0

emergency_boost_mp_offset=2.68

emergency_boost_gain_offset=0.54

fuel_air_auto_mixture=1

auto_ignition=0

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=1.0

propeller_type=0

propeller_diameter=10.1

propeller_blades=4

propeller_moi=32.8

beta_max=65

beta_min=15

min_gov_rpm=400

prop_tc=0.01

gear_reduction_ratio=1.6

fixed_pitch_beta=0

low_speed_theory_limit=80

prop_sync_available=0

prop_deice_available=0

prop_feathering_available=1

prop_auto_feathering_available=0

min_rpm_for_feather=70.0

beta_feather=88.5

power_absorbed_cf=0.9

defeathering_accumulators_available=0

prop_reverse_available=0.0

minimum_on_ground_beta=0.0

minimum_reverse_beta=0.0

 

[ground_reaction]

main_gear_static_compression=0.3

center_gear_static_compression=0.33

main_gear_damping_ratio=0.9

center_gear_damping_ratio=0.8

 

[electrical]

max_battery_voltage = 24.0

generator_alternator_voltage = 28.0

max_generator_alternator_amps = 60.0

 

[folding_wings]

wing_fold_system_type = 1 ;0=None

fold_rates = 1.0,1.0 ;Percent per second

 

[contact_points]

 

//0 Class

//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,-16.6, 0.0, -1.8, 1574, 0, 0.5, 45, 0.5, 2.5, 0.8, 0,0, 0.0, 0, 0, 0

point.1=1, 2.8, -3.1, -6.4, 1574, 1, 1.3, 0, 0.5, 2.5, 0.8, 3.5, 9.0, 2, 128,143

point.2=1, 2.8, 3.1, -6.4, 1574, 2, 1.3, 0, 0.5, 2.5, 0.8, 4.5, 6.5, 3, 128,143

 

point.3=2, 0.0, -16.5, 0.8, 787, 0, 0.0, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0, 0

point.4=2, 0.0, 16.5, 0.8, 787, 0, 0.0, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0, 0

point.5=2,-19.7, 0.0, 1.8, 787, 0, 0.0, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0, 0

point.6=2, 7.4, 0.0, -3.7, 787, 0, 0.0, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0, 0

point.7=2, 0.0, -16.5, -0.1, 787, 0, 0.0, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 7, 0, 0

 

 

point.8=5, 7.1, 0.0, -0.5, 1600, 0,0.0,10,0.4,2.5,1,0.2,0.2,4

 

static_pitch=13.18

static_cg_height=4.850

gear_system_type=1

 

[flaps.0]

type=1 // 1 - tail, 2 - lead

span-outboard=0.4 // 0.0 .. 1.0

extending-time=5 // seconds

flaps-position.0=0 // degrees, KIAS

flaps-position.1=15,193 // degrees, KIAS

flaps-position.2=25,165 // degrees, KIAS

flaps-position.3=33,137 // degrees, KIAS

flaps-position.4=45,109 // degrees, KIAS

damaging-speed=177 // KIAS

blowout-speed=214 // KIAS

 

 

[Views]

eyepoint=-2.5, 0.0, 2.00

 

 

 

[fuel]

Center1 = -0.8, 0.0, -1.0, 105.4, 0.4

External1= 2.3, 0.0, -4.4, 79.1, 0.1

fuel_type=1.0

number_of_tank_selectors=1

electric_pump=0

 

[airplane_geometry]

wing_area=198

wing_span=32

wing_root_chord=5.75

wing_dihedral=6.9

wing_incidence=0.9

wing_twist=-0.5

oswald_efficiency_factor=1.0

wing_winglets_flag=0

wing_sweep=0.0

wing_pos_apex_lon=0.0

wing_pos_apex_vert=0.0

 

htail_area=28.0

htail_span=10.0

htail_pos_lon=-15.2

htail_pos_vert=0.0

htail_incidence=0.0

htail_sweep=0.0

 

vtail_area=25.0

vtail_span=5.7

vtail_sweep=0.0

vtail_pos_lon=-16.6

vtail_pos_vert=2.75

 

elevator_area=19.0

aileron_area=19.0

rudder_area=19.0

 

elevator_up_limit=28.0

elevator_down_limit=28.0

aileron_up_limit=16.9

aileron_down_limit=16.8

rudder_limit=29.9

elevator_trim_limit=14.3

spoiler_limit=16.3

 

spoilerons_available=0

aileron_to_spoileron_gain=0.0

min_ailerons_for_spoilerons=0.0

min_flaps_for_spoilerons=0.0

auto_spoiler_available=0

spoiler_extension_time=0.3

positive_g_limit_flaps_up=8.5

positive_g_limit_flaps_down=7.0

negative_g_limit_flaps_up=-5.5

negative_g_limit_flaps_down=-4.6

 

[brakes]

toe_brakes_scale=0.7

parking_brake=1

 

[gear_warning_system]

gear_warning_available=1

pct_throttle_limit=0.2

flap_limit_power=40.1

flap_limit_idle=26.3

 

 

[GeneralEngineData]

engine_type=0

Engine.0=7.5,0.0,0.0

fuel_flow_scalar=1.0

min_throttle_limit=0.0

 

[Reference Speeds]

flaps_up_stall_speed=88

full_flaps_stall_speed=70

cruise_speed=180

max_indicated_speed=406

 

[keyboard_response]

elevator=0,0

aileron=0,0

rudder=0,0

 

 

 

 

[hydraulic_system]

electric_pumps=0

engine_map=1,0,0,0

normal_pressure=6.9

 

[stall_warning]

type=1

stick_shaker=1

 

[attitude_indicators]

attitude_indicator.0=1

 

[turn_indicators]

turn_indicator.0=1,0

 

[direction_indicators]

direction_indicator.0=1,0

 

[pitot_static]

pitot_heat=1.0

 

[vacuum_system]

max_pressure=5.0

vacuum_type=1

electric_backup_pressure=0.0

engine_map=1

 

[pneumatic_system]

max_pressure=0.0

bleed_air_scalar=0.0

 

[deice_system]

structural_deice_type=0

 

[sMOKESYSTEM]

//reference datum vertical, longitudinal, lateral

smoke.0= -10.0, 0.0, -0.5, fx_su_vaportrail.fx

 

[EFFECTS]

wake = fx_wake

water = fx_spray

dirt = fx_tchdrt

concrete = fx_sparks

touchdown = fx_tchdwn

startup=fx_engstrt

 

[LIGHTS]

//1 Longitudinal - minus rear (feet)

//2 Lateral - minus left (feet)

//3 elevation - minus lower (feet)

 

//#1=beacon #2=strobe #3=nav #10=reheat

//#4=cockpit #5=landing #6=taxi

//#7=recog #8=wing #9=logo

//---------------originals----------------------------

light.0=4, 0.8, -16.0, -0.2, fx_navred

light.1=4, 0.8, 16.0, -0.2, fx_navgre

light.2=4, -4.6, 0.0, -1.2, fx_beacon

light.3=4, -20.1, 0.0, 1.4, fx_strobeh

 

 

/---------- ExhaustFlames--------uses wing/taxi/logo

//index,type, long, lat, vert, fx_filename

light.4=8, 2.5, -1.5, -0.9, fx_V12_IDLE_port

light.5=8, 2.5, 1.5, -0.9, fx_V12_IDLE_starb

light.6=6, 2.5, -1.5, -0.9, fx_V12_MAX_port

light.7=6, 2.5, 1.5, -0.9, fx_V12_MAX_starb

light.8=9, 2.5, -1.6, -0.9, fx_V12_Exhaust

light.9=9, 2.5, 1.6, -0.9, fx_V12_Exhaust

 

//------------ Guns ----------------------uses strobe

light.10=2, 4.0, -0.5, 1.6, fx_Wing_Guns

light.11=2, 4.0, 0.5, 1.6, fx_Wing_Guns

light.12=2, 3.5, 7.5, -0.8, fx_Wing_Guns

light.13=2, 3.5, -7.5, -0.8, fx_Wing_Guns

 

 

 

[autopilot]

autopilot_available=1

flight_director_available=0

default_vertical_speed=700

autothrottle_available=1

autothrottle_arming_required=0

autothrottle_takeoff_ga=0

autothrottle_max_rpm=90

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

max_pitch_velocity_hi_alt_breakpoint=28000

max_bank=25.0

max_bank_acceleration=1.8

max_bank_velocity=3.0

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=0.0

 

 

 

 

 

[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=6000 ; 0 - 10000

gear_bump_left_direction=35500 ; 0 - 35999 degrees

gear_bump_left_duration=250000 ; 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=3250 ; 0 - 10000

ground_bumps_angle1=8900 ; 0 - 35999 degrees

ground_bumps_intercept1=5.0

ground_bumps_slope1=0.48

ground_bumps_magnitude2=750 ; 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

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WELL thanks to everyone who helped me get this problem resolved.

 

It looks like moving the p-factor to the left solved the problem. All the ME 109s now track down the center of the runway.

 

I never thought of the p-factor as I moved all the settings to the right side and have been using the sim that way.

 

 

 

 

I really did use right rudder but the high amount of torque over come the rudder

Edited by Rnglgdj
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