netřeba,
při každým !!
Tady bude problém, ale už jsem měnil a měnil všechno možný, zkoušel a jsem z toho jelen už.
[WEIGHT_AND_BALANCE]
empty_weight = 394088.0 // 3-Class
max_gross_weight = 875000.0 // 800, 833, 850, 870, 875 x 10^3 lbs [+2000 for max ramp]
max_landing_weight = 630000.0 // 574, 630 x 10^3 lbs
max_zerofuel_weight = 542500.0 // 535, 542.5 x 10^3 lbs
CG_forward_limit=0.130 // 11% 572000-775000 lbs
CG_aft_limit=0.331
// WARNING : DO NOT EDIT !
reference_datum_position = 97.0, 0, 0 // (feet) Boeing Section2.0 reference position (RefPos)
empty_weight_CG_position = -97.85, 0, 0 // (feet) from RefPos 19.75% MAC
max_number_of_stations = 50
station_load.0 = 72600.0, -98.41, 0 ,0
station_load.1 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.2 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.3 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.4 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation"
;Moments of Inertia
empty_weight_pitch_MOI = 17018677.379279
empty_weight_roll_MOI = 15962454.863936
empty_weight_yaw_MOI = 16890566.121607
empty_weight_coupled_MOI = 2048.0 |
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