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ISVA/USN flyable mods


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I fly both in 1.5.2 fine

 

with the F15 C cockpit?

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  • 2 weeks later...

Hi and thanks for sharing the new link.

 

I've tested the A-7e from there and the 3d model is awesome. The mod seems very stable too. It's clearly a great job done to add this aircraft.

 

But I have a question if anyone has an answer: the configuration files in the "entry folder" do not have the .lua extension and thus are more or less impossible to edit. Do you know if there is a way to edit them anyway ? I ask this because I would like to tweak the flight model a little.

 

Best regards,

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Hi and thanks for sharing the new link.

 

I've tested the A-7e from there and the 3d model is awesome. The mod seems very stable too. It's clearly a great job done to add this aircraft.

 

But I have a question if anyone has an answer: the configuration files in the "entry folder" do not have the .lua extension and thus are more or less impossible to edit. Do you know if there is a way to edit them anyway ? I ask this because I would like to tweak the flight model a little.

 

Best regards,

 

Hi!

Try this file...

 

Pitch and Bank rate corrected.

Induced drag corrected.

Flaps drag and lift force corrected.

Engine data corrected.

 

 

SFM_Data = {
   aerodynamics = 
       {
           Cy0            =    0,            -- zero AoA lift coefficient
           Mzalfa        =    4.65,        -- coefficients for pitch agility
           Mzalfadt        =    0.8,        -- coefficients for pitch agility
           kjx            =    2.15,        
           kjz            =    0.00125,    
           Czbe            =    -0.016,        -- coefficient, along Z axis (perpendicular), affects yaw, negative value means force orientation in FC coordinate system
           cx_gear        =    0.03,    -- coefficient, drag, gear
           cx_flap        =    0.06,    -- coefficient, drag, full flaps
           cy_flap        =    0.3,        -- coefficient, normal force, lift, flaps
           cx_brk        =    0.14,        -- coefficient, drag, breaks
           table_data = 
           {        --    M        Cx0            Cya            B        B4        Omxmax    Aldop    Cymax
               [1] =     {0,    0.0165,        0.0817,        0.0921,    0,        0.5,    30,        1.10},
               [2] =     {0.1,    0.0165,        0.0817,        0.0921,    0,        0.6,    30,        1.10},
               [3] =     {0.2,    0.0165,        0.0817,        0.0921,    0,        1.0,    28,        1.10},
               [4] =     {0.3,    0.0167,        0.0817,        0.0921,    0,        1.0,    28,        1.10},
               [5] =     {0.4,    0.0169,        0.0817,        0.0921,    0,        2.0,    26,        1.10},
               [6] =     {0.4,    0.0170,        0.0817,        0.0921,    0,        2.0,    26,        1.10},
               [7] =     {0.6,    0.0170,        0.0872,        0.0921,    0,        2.4,    24,        1.10},
               [8] =     {0.7,    0.0170,        0.0872,        0.3,    0.052,    2.6,    20,        1.09},
               [9] =     {0.8,    0.0172,        0.0872,        0.3,    0.052,    2.8,    18,        1.08},
               [10] =     {0.9,    0.0173,        0.0855,        0.324,    0.0536,    3.0,    14,        1.07},
               [11] =     {1.0,    0.0365,        0.0855,        0.348,    0.0552,    3.0,    12,        1.06},
               [12] =     {1.1,    0.0750,        0.0860,        0.372,    0.0568,    2.5,    6,        1.04},
               [13] =     {1.2,    0.0750,        0.0830,        0.396,    0.0584,    2.2,    4,        1.02},
               [14] =     {1.3,    0.0750,        0.0770,        0.42,    0.06,    1.5,    2,        1.00},
               [15] =     {1.5,    0.0750,        0.0620,        0.4886,    0.06,    1.2,    2,        0.90},
           }, -- end of table_data
           -- M - Mach number
           -- Cx0 - Coefficient, drag, profile, of the airplane
           -- Cya - Normal force coefficient of the wing and body of the aircraft in the normal direction to that of flight. Inversely proportional to the available G-loading at any Mach value. (lower the Cya value, higher G available) per 1 degree AOA
           -- B - Polar quad coeff
           -- B4 - Polar 4th power coeff
           -- Omxmax - roll rate, rad/s
           -- Aldop - Alfadop Max AOA at current M - departure threshold
           -- Cymax - Coefficient, lift, maximum possible (ignores other calculations if current Cy > Cymax)
       }, -- end of aerodynamics
       
       engine = 
       {
           Nmg        =    54.0,    -- RPM at idle
           MinRUD    =    0,        -- Min state of the throttle
           MaxRUD    =    1,        -- Max state of the throttle
           MaksRUD    =    0.91,    -- Military power state of the throttle
           ForsRUD    =    0.99,    -- Afterburner state of the throttle
           typeng    =    1,        
           hMaxEng    =    15,        -- Max altitude for safe engine operation in km
           dcx_eng    =    0.0144,    -- Engine drag coeficient
           cemax    =    1.24,    -- not used for fuel calulation , only for AI routines to check flight time ( fuel calculation algorithm is built in )
           cefor    =    1.24,    -- not used for fuel calulation , only for AI routines to check flight time ( fuel calculation algorithm is built in )
           dpdh_m    =    2500,    -- altitude coefficient for max thrust
           dpdh_f    =    2500,    --  altitude coefficient for AB thrust
           table_data = 
           {
               [1] =     {0,    67820,    500000},
               [2] =     {0.1,    68020,    250000},
               [3] =     {0.2,    68600,    68600},
               [4] =     {0.3,    69540,    69540},
               [5] =     {0.4,    70780,    70780},
               [6] =     {0.5,    72240,    72240},
               [7] =     {0.6,    73810,    73810},
               [8] =     {0.7,    75360,    75360},
               [9] =     {0.8,    76730,    76730},
               [10] =     {0.9,    77750,    77750},
               [11] =     {1.0,    78100,    78100},
               [12] =     {1.1,    26150,    26150},
               [13] =     {1.2,    19680,    19680},
               [13] =     {1.3,    12540,    12540},
               [14] =     {1.4,     4870,     4870},
               [15] =     {1.5,        0,        0},
           }, -- end of table_data
       }, -- end of engine
   },

 


Edited by Morkva_55

su-24.gif

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Is the air to ground load out updated too? On your photos are dual Zuni racks - can't find them?!

 

Yes, you can't. This is part of the new F/A-18C mod by ISVA.

 

New mod will be include some new weapons declaration:

 

- LAU-115C 2 x LAU-127 AIM-120C

- LAU-115C 2 x LAU-127 AIM-120B

- LAU-115C AIM-7M

- LAU-115C 2 x LAU-7 AIM-9P

- LAU-115C 2 x LAU-7 AIM-9M

- LAU-115C 2 x LAU-7 AIM-9X

- LAU-127 AIM-120C

- LAU-127 AIM-120B

- LAU-127 AIM-120B

- LAU-127 AIM-9P

- LAU-127 AIM-9M

- LAU-127 AIM-9X

- BLU-107B Durandal

- BRU-55/A 2 x BLU-107B Durandal

- LAU-10 x 4 Zuni MK71 motor MK 32 warhead (Anti-Tank/Anti-Personnel) 2 rocket is overkill for T-90...

- BRU-55/A 2 x LAU-10 x 8 Zuni MK 32

- BRU-55/A 2 x CBU-97

- ALQ-167 Jammer Pod

 

New system controls for external model animation:

 

- AutoFlaps system on stall, high AOA flight conditions

- Auto SpeedBrake retraction IAS<200 Kts

- LE and TE Flaps driven by AOA input data in cruise configuration

- LE and TE Flaps fixed position in landing configuration, Aileron droop

- G-Limiter (bugged but sometimes works)

- Wings damage and destruction on High-G maneuvers G>10 (in test, but funny thing). Who said it would be easy? )))

 

And one but most actual thing!

 

- F/A-18C now uses modded F-15C input controls - so no more headashes with Su-33 brain damaged input configuration.

That's all the news so far.


Edited by Morkva_55

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But will we ever see this in public?

 

Yes of course.

 

And one more thing - this mod will be available with optional AFM also for ashore operation only.

Unfortunately AFM makes impossible takeoff and recovery from the carrier due the absense of FM contact model with the deck surface.

 

 

Current mood...

 

Defender of the Fatherland Day

 

358013924.jpg

 


Edited by Morkva_55

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Happy to hear this!!

 

& one more question. are the new zuni racks animated? Will they be empty when the rockets are fired?


Edited by Foxbeard

__________________

 

Windows 7 Ult 64 Bit | Intel Core i5-3570 | 16GB DDR3-2133 | GTX 770

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