Modifications for C152, G36, 208b and 748i

Modifications for C152, G36, 208b and 748i

It will fly pretty close to the real one. You need to have also FSUPIC.

Backup and edit flight_model 

//152
[WEIGHT_AND_BALANCE]

empty_weight_pitch_MOI = 775.13  //1717 ; Empty pitch moment of inertia, Jxx (SLUG SQ FEET)
empty_weight_roll_MOI = 644.88  //1388 ; Empty roll moment of inertia, Jzz (SLUG SQ FEET)
empty_weight_yaw_MOI = 1160.41  //2770 ; Empty yaw moment of inertia, Jyy (SLUG SQ FEET)
empty_weight_coupled_MOI = 10 ; Empty transverse moment of inertia, Jyz (SLUG SQ FEET)

[FLIGHT_TUNING]
******************************************************************
aileron_effectiveness = 1
aileron_maxangle_scalar = 0.6
roll_stability = 1

elevator_effectiveness = 0.5
elevator_maxangle_scalar = 1
pitch_stability = 1
elevator_trim_effectiveness = 1.3

rudder_effectiveness = 0.5
rudder_maxangle_scalar = 0.66
yaw_stability = 1
********************************************************************

In FSUPIC

Flight Control Response curve for:
Aileron set @ 7
Elevator set @ 8
Rudder set @ 7

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//asobo-aircraft-bonanza-g36

[WEIGHT_AND_BALANCE]
empty_weight_pitch_MOI = 1016.62  //3749 ; Empty pitch moment of inertia, Jxx (SLUG SQ FEET)
empty_weight_roll_MOI = 652.62  //2352 ; Empty roll moment of inertia, Jzz (SLUG SQ FEET)
empty_weight_yaw_MOI = 1341.55  //5838 ; Empty yaw moment of inertia, Jyy (SLUG SQ FEET)
empty_weight_coupled_MOI = 100 ; Empty transverse moment of inertia, Jyz (SLUG SQ FEET)

[FLIGHT_TUNING]
******************************************************************
aileron_effectiveness = 1
aileron_maxangle_scalar = 0.6
roll_stability = 1

elevator_effectiveness = 0.2  
elevator_maxangle_scalar = 1
pitch_stability = 1.2
elevator_trim_effectiveness = 1.33

rudder_effectiveness = 0.5
rudder_maxangle_scalar = 0.66
yaw_stability = 1
********************************************************************

In FSUPIC

Flight Control Response curve for:
Aileron set @ 7
Elevator set @ 6
Rudder set @ 7

XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX

Asobo_208B_GRAND_CARAVAN_EX

[FLIGHT_TUNING]
******************************************************************
aileron_effectiveness = 1
aileron_maxangle_scalar = 0.6
roll_stability = 1

elevator_effectiveness = 0.2
elevator_maxangle_scalar = 1
pitch_stability = 2
elevator_trim_effectiveness = 1.3

rudder_effectiveness = 0.5
rudder_maxangle_scalar = 0.66
yaw_stability = 1
********************************************************************

cruise_lift_scalar = 1
parasite_drag_scalar = 1
induced_drag_scalar = 1.15
flap_induced_drag_scalar = 1.15

aileron_trim_effectiveness = 1
rudder_trim_effectiveness = 1.5
hi_alpha_on_roll = 0
hi_alpha_on_yaw = 0
p_factor_on_yaw = 1
torque_on_roll = 1
gyro_precession_on_roll = 1
gyro_precession_on_yaw = 1
engine_wash_on_roll = 1 ; Torque effect
rudder_engine_wash_on_roll = 2.0 ; Torque effect

[WEIGHT_AND_BALANCE]

empty_weight_pitch_MOI = 28262 ; Empty pitch moment of inertia, Jxx (SLUG SQ FEET)
empty_weight_roll_MOI = 13561 ; Empty roll moment of inertia, Jzz (SLUG SQ FEET)
empty_weight_yaw_MOI = 38012 ; Empty yaw moment of inertia, Jyy (SLUG SQ FEET)
empty_weight_coupled_MOI = 500 ; Empty transverse moment of inertia, Jyz (SLUG SQ FEET)

In FSUPIC

Flight Control Response curve for:
Aileron set @ 7
Elevator set @ 8
Rudder set @ 7

XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX

748I

[FLIGHT_TUNING]
cruise_lift_scalar = 1
parasite_drag_scalar = 1
induced_drag_scalar = 1
flap_induced_drag_scalar = 1
******************************************************************
aileron_effectiveness = 1
aileron_maxangle_scalar = 0.6
roll_stability = 1

elevator_effectiveness = 0.2
elevator_maxangle_scalar = 1
pitch_stability = 3.0  
elevator_trim_effectiveness = 1.7  

rudder_effectiveness = 0.5
rudder_maxangle_scalar = 0.66
yaw_stability = 1
********************************************************************
aileron_trim_effectiveness = 1
rudder_trim_effectiveness = 1
hi_alpha_on_roll = 0
hi_alpha_on_yaw = 0
p_factor_on_yaw = 0
torque_on_roll = 0
gyro_precession_on_roll = 0
gyro_precession_on_yaw = 0
engine_wash_on_roll = 0 ; Torque effect
wingflex_scalar = 0.5
wingflex_offset = 0

[WEIGHT_AND_BALANCE]

empty_weight_pitch_MOI = 37505925.20   //////////76427903; Empty pitch moment of inertia, Jxx (SLUG SQ FEET)
empty_weight_roll_MOI = 13079808.20   //////////19300696 ; Empty roll moment of inertia, Jzz (SLUG SQ FEET)
empty_weight_yaw_MOI = 35505696.65   ///////////89315555 ; Empty yaw moment of inertia, Jyy (SLUG SQ FEET)
empty_weight_coupled_MOI = 10000 ; Empty transverse moment of inertia, Jyz (SLUG SQ FEET)

In FSUPIC

Flight Control Response curve for:
Aileron set @ 7
Elevator set @ 8
Rudder set @ 7