plane: adjusted parameters
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1 changed files with 4 additions and 4 deletions
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@ -56,9 +56,9 @@ local lift = function(angle)
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return 1.68429 * math.exp(-math.pow(angle / math.pi * 180.0 -17.3801, 2.0) / (2.0 * math.pow(15.0, 2.0)))
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end
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local fwd_frict_coeff = 0.5
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local nor_frict_coeff = 0.9
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local tail_frict_coeff = 0.5
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local fwd_frict_coeff = 0.1
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local nor_frict_coeff = 0.8
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local tail_frict_coeff = 0.4
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local tail_area = 5.0
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local turn_coeff = 500.0
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local wing_lift = 0.5
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@ -67,7 +67,7 @@ local decel_speed = 400.0
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local max_motorPower = ENGINE_MAX
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local head_area = 1.0
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local plane_area = 10.0
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local motor_speed_ratio = 100.0
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local motor_speed_ratio = 80.0
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local out_of_bounds_coeff_multiplier = 10.0
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