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feat(FM): Temporary fix for excessive ground effect and poor control …
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…response.
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747-4EVER committed Jan 25, 2022
1 parent 114c29b commit ba518fd
Showing 1 changed file with 2 additions and 2 deletions.
4 changes: 2 additions & 2 deletions salty-747/SimObjects/Airplanes/Asobo_B747_8i/flight_model.cfg
Original file line number Diff line number Diff line change
Expand Up @@ -360,7 +360,7 @@ elevator_elasticity_table = 0:1, 100:1, 250:0.9, 400:0.33, 600:0.25
aileron_elasticity_table = 0:1, 100:1, 250:0.9, 400:0.33, 600:0.25
rudder_elasticity_table = 0:1, 100:1, 250:0.9, 400:0.33, 600:0.25
elevator_trim_elasticity_table = 0:1, 100:1, 250:0.9, 400:0.33, 600:0.25
controls_reactivity_scalar = 0.25
controls_reactivity_scalar = 0.5

[AERODYNAMICS]
lift_coef_pitch_rate = -109.70206 ; The change in lift per change in pitch rate
Expand Down Expand Up @@ -406,7 +406,7 @@ yaw_moment_delta_rudder_trim_scalar = 0.95632 ; Change in yaw moment due to rudd
compute_aero_center = 0
aero_center_lift = -14.00000
lift_coef_aoa_table = -3.15:0, -0.8:-1.154, -0.4:-0.928, -0.2:-0.781, -0.1:-0.372, 0:0.250, 0.20:1.215, 0.23:1.293, 0.26:1.314, 0.29:1.117, 0.31:1.049, 0.4:0.941, 0.8:1.183, 3.15:0
lift_coef_ground_effect_mach_table = 0.054:1.25
lift_coef_ground_effect_mach_table = 0.054:1.05
lift_coef_mach_table = 0:1
lift_coef_delta_elevator_mach_table = 0:0
lift_coef_daoa_mach_table = 0:0
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