Hello.
After some tests, i share you a new modification for the flightmodel config file:
From the original file:
[WEIGHT_AND_BALANCE]
empty_weight_CG_position = 0.199,0,0 ; Position of airplane empty weight CG relative to reference datum (FEET), z, x, y
[FUSELAGE_AERODYNAMICS]
vstab_incidence = 7 ; degrees , incidence of vertical stabilizer
vstab_lift_coef = 2 ; lift coef , slope of lift coefficient over aoa for vertical stabilizer
[HELICOPTER]
cyclic_roll_control_scalar = 2.2 ; scalar , scales roll cyclic controls ( ! optional ! )
cyclic_pitch_control_scalar = 3.8 ; scalar , scales pitch cyclic controls (! optional !)
[MAINROTOR]
static_bank_angle = -6 ; degrees , neutral cyclic input angle
cyclic_bank_centre = -0.05
[SECONDARYROTOR]
blade_beta_input_max = 14 ; degrees , rotor beta at maximum rudder input
blade_beta_input_min = 2.4 ; degrees , rotor beta at minimum rudder input