FIREFLY FOR FALCON BMS J10MOD
来源:百度文库 编辑:超级军网 时间:2024/04/29 14:32:47
http://player.youku.com/player.php/sid/XODQzOTA5MzI0/v.swf
从@雷纳尔 那里拿到了这个MOD,起飞降落,恶意满满http://player.youku.com/player.php/sid/XODQzOTA5MzI0/v.swf
从@雷纳尔 那里拿到了这个MOD,起飞降落,恶意满满
从@雷纳尔 那里拿到了这个MOD,起飞降落,恶意满满http://player.youku.com/player.php/sid/XODQzOTA5MzI0/v.swf
从@雷纳尔 那里拿到了这个MOD,起飞降落,恶意满满
还好开无敌了
看起来 你们很爽呀
这是打CS出身?
....这外模怎么样?
biller 发表于 2014-12-12 13:07
....这外模怎么样?
外模比较一般、舱内有一部分仿照F16(不仿就不能冷启)、气动一塌糊涂。
顺道补一下从FreeFalcon转过来的歼十OFM
- #
- #A-G Weapons release profile added April 19, 2004 JimG
- #Renard modified from Free Falcon J10.dat
- #
- # SIMULATION INPUT PANEL
- #
- # INPUT MASS AND GEOMETRIC PROPERTIES:
- 19884 # Empty Weight (lbs)
- 437 # Reference Area
- 7900 # Internal Fuel
- #
- #
- # ANGLE OF ATTACK AND SIDESLIP LIMITS
- 35 # AOA Max
- -15 # AOA Min
- 15 # Beta Max
- -15 # Beta Min
- 9 # Max G
- 190 # Max Roll
- 250 # Min Vcas
- 900 # Max Vcas
- 420 # Corner Vcas
- 12 # Theta Max
- 3 # Num Gear
- # Gear X. Y. Z. Rng
- 15.9 0 8.2 100
- 28.6 -2.6 7.3 100
- 28.6 2.6 7.3 100
- #
- # Physical data
- 25.77 # CG Loc
- 46.85 # Length
- 27.16 # Span
- 3 # Fus Radius
- 13.6 # Tail Ht
- #
- # End of Airframe data
- #
- #
- #
- # BASIC AERODYNAMIC COEFFICIENTS
- #
- #
- # MACH BREAKPOINTS
- #
- 10 # Num MACH
- 0 0.2 0.4 0.69
- 0.83 0.89 0.95 1.2 1.6
- 2.5
- #
- # ALPHA BREAKPOINTS
- #
- 12 # Num Alpha
- -20 -10 -5 0
- 5 10 15 20 25
- 30 35 40
- #
- # LIFT COEFFICIENT CL
- #
- 1 # Table Multiplier
- #
- # Mach 0.000
- -1.09716 -0.83076 -0.36744 -0.06 0.198 0.42 0.654 0.83456 1.04864 1.252 1.348 1.336
- #
- # Mach 0.200
- -1.09716 -0.83076 -0.36744 -0.06 0.198 0.42 0.654 0.83456 1.04864 1.252 1.348 1.336
- #
- # Mach 0.400
- -1.09716 -0.83076 -0.36744 -0.06 0.198 0.42 0.654 0.93456 1.14864 1.452 1.548 1.536
- #
- # Mach 0.690
- -1.09716 -0.83076 -0.36744 -0.06 0.198 0.42 0.654 0.93456 1.14864 1.452 1.548 1.536
- #
- # Mach 0.830
- -0.939 -0.714 -0.3246 -0.06 0.173 0.374 0.575 0.80492 0.97162 1.22852 1.33182 1.32792
- #
- # Mach 0.890
- -0.97 -0.7244 -0.3434 -0.06 0.18 0.375 0.575 0.84088 1.00698 1.26258 1.36808 1.37248
- #
- # Mach 0.950
- -1.0322 -0.7444 -0.3634 -0.08 0.175 0.385 0.68104 0.95714 1.12324 1.37884 1.48434 1.48874
- #
- # Mach 1.200
- -1.0322 -0.7634 -0.3866 -0.1 0.15 0.40804 0.74834 1.02474 1.19674 1.45524 1.55414 1.56414
- #
- # Mach 1.600
- -1.0322 -0.7634 -0.3866 -0.1 0.15 0.40804 0.74834 1.02474 1.19674 1.45524 1.55414 1.56414
- #
- # Mach 2.500
- -1.0322 -0.7634 -0.386 -0.1 0.15 0.40804 0.74834 1.02474 1.19674 1.45524 1.55414 1.56414
- #
- # DRAG COEFFICIENT CD
- #
- 0.66666 # Table Multiplier
- #
- # Mach 0.000
- 0.2381 0.1882 0.0759 0.0223 0.0259 0.0353 0.0827333 0.176667 0.349733 0.5784 0.669127 0.878
- #
- # Mach 0.200
- 0.1945 0.15461 0.0647079 0.0228899 0.02595 0.0353 0.0827333 0.183333 0.359783 0.580913 0.67794 0.947713
- #
- # Mach 0.400
- 0.1945 0.15461 0.0647079 0.0228899 0.02595 0.0353 0.0827333 0.183333 0.359783 0.580913 0.67794 0.947713
- #
- # Mach 0.690
- 0.2046 0.164864 0.0706953 0.0235326 0.0243 0.0415 0.09805 0.21246 0.38537 0.614628 0.804227 1.01579
- #
- # Mach 0.830
- 0.2048 0.165003 0.0708347 0.0236719 0.02446 0.04558 0.11275 0.242707 0.413821 0.643079 0.83268 1.04424
- #
- # Mach 0.890
- 0.2077 0.161755 0.0738287 0.024244 0.0246 0.0485 0.11225 0.262248 0.429649 0.663252 0.933667 1.05351
- #
- # Mach 0.950
- 0.2076 0.16167 0.073742 0.0243388 0.0245 0.0495 0.16208 0.325518 0.492919 0.72652 0.99694 1.11678
- #
- # Mach 1.200
- 0.2198 0.150914 0.0805253 0.0210382 0.0355 0.04402 0.147503 0.312995 0.46 0.778927 1.03939 1.1747
- #
- # Mach 1.600
- 0.2198 0.150914 0.0805253 0.0203715 0.038 0.045228 0.128933 0.2662 0.394767 0.907927 1.16839 1.30372
- #
- # Mach 2.500
- 0.2188 0.149914 0.0795253 0.0200382 0.0375 0.0366853 0.12 0.259684 0.391267 0.92562 1.18608 1.32141
- #
- # SIDE FORCE DERIVATIVE CY-BETA
- #
- 1 # Table Multiplier
- #
- # Mach 0.00
- -0.0109 -0.0166 -0.0182 -0.0192 -0.0187 -0.0163
- -0.0176 -0.0164 -0.0158 -0.0141 -0.009 -0.011
- #
- # Mach 0.20
- -0.0109 -0.0166 -0.0182 -0.0192 -0.0187 -0.0163
- -0.0176 -0.0164 -0.0158 -0.0141 -0.009 -0.016
- #
- # Mach 0.40
- -0.0109 -0.0166 -0.0182 -0.0192 -0.0187 -0.0163
- -0.0176 -0.0164 -0.0158 -0.0141 -0.009 -0.016
- #
- # Mach 0.69
- -0.0122 -0.021 -0.028 -0.0286 -0.03 -0.025
- -0.0267 -0.0223 -0.0215 -0.0187 -0.0172 -0.017
- #
- # Mach 0.83
- -0.0172 -0.027 -0.033 -0.035 -0.0333 -0.0321
- -0.0288 -0.0254 -0.0231 -0.0207 -0.0188 -0.0171
- #
- # Mach 0.89
- -0.01725 -0.0271 -0.03325 -0.03525 -0.03355 -0.03235
- -0.029 -0.0257 -0.02355 -0.02085 -0.0194 -0.01715
- #
- # Mach 0.95
- -0.017275 -0.02715 -0.033375 -0.035375 -0.033675 -0.032475
- -0.0291 -0.02585 -0.023775 -0.020925 -0.0197 -0.0172
- #
- # Mach 1.20
- -0.0173 -0.0272 -0.0335 -0.0355 -0.0338 -0.0326
- -0.0292 -0.026 -0.024 -0.021 -0.02 -0.0172
- #
- # Mach 1.60
- -0.0173 -0.0272 -0.0335 -0.0355 -0.0338 -0.0326
- -0.0292 -0.026 -0.024 -0.021 -0.02 -0.0161
- #
- # Mach 2.50
- -0.0162 -0.0194 -0.0194 -0.0215 -0.0216 -0.0214
- -0.0215 -0.0205 -0.0179 -0.0153 -0.0105 -0.0161
- # End of Aero Data
- #
- #
- # PROPULSION DATA
- #
- 1 # Thrust multiplier
- 0.6 # Fuel Flow Multiplier
- #
- # MACH BREAKPOINTS
- #
- 13 # Number of Mach Breaks
- 0 0.2 0.4 0.6 0.8 1
- 1.2 1.4 1.6 1.8 2 2.4 2.5
- #
- # ALTITUDE BREAKPOINTS
- #
- 8 # Number of Alt Break Points
- 0 10000 20000 30000 36000 40000
- 50000 70000
- #
- # THRST1 - THRUST AT IDLE (THROTL = 0.00)
- #
- # Alt 0
- 0 -800 -1700 -2200 -3300 -4000 -4900 -5900 -6700 -7700 -8600 -10800 -10800
- #
- # Alt 10000
- 0 -400 -1100 -1650 -2250 -2800 -3450 -4050 -4600 -5100 -5750 -7400 -7400
- #
- # Alt 20000
- 0 -370 -740 -1100 -1480 -1850 -2230 -2550 -2900 -3330 -3700 -4625 -4625
- #
- # Alt 30000
- 0 -230 -450 -690 -920 -1150 -1380 -1600 -1850 -2075 -2300 -2880 -2880
- #
- # Alt 36000
- 0 -160 -340 -500 -675 -850 -1000 -1190 -1360 -1520 -1700 -2125 -2125
- #
- # Alt 40000
- 0 -140 -275 -415 -550 -690 -835 -975 -1115 -1250 -1390 -1740 -1740
- #
- # Alt 50000
- 0 -80 -170 -255 -345 -430 -515 -600 -690 -775 -860 -1075 -1075
- #
- # Alt 70000
- 0 -40 -85 -125 -165 -210 -250 -290 -335 -375 -420 -525 -525
- #
- # THRST2 - THRUST AT MIL POWER (THROTL = 1.00)
- #
- # Alt 0
- 16779 15520.6 16107.8 17198.5 18037.4 18474.8 18000 18000 18000 18000 18000 18000 18000
- #
- # Alt 10000
- 12500.4 11325.8 11158 12584.3 14262.2 14861.9 12000 10000 10000 10000 10000 10000 10000
- #
- # Alt 20000
- 8389.5 7298.87 6711.6 8389.5 9647.92 11495.4 10900 10300 10000 10000 10000 10000 10000
- #
- # Alt 30000
- 5872.65 5453.17 5033.7 5285.38 6292.13 6979.35 7100 6600 6600 6600 6600 6000 6000
- #
- # Alt 36000
- 4194.75 4152.8 4068.91 4194.75 4614.23 5994.03 6100 5500 5500 5000 5000 5000 5000
- #
- # Alt 40000
- 3355.8 3271.91 2936.32 3188.01 4110.85 4598.16 4444 4000 4000 4000 4000 4000 4000
- #
- # Alt 50000
- 2097.38 2013.48 1988.31 2105.76 2516.85 2700 2200 2000 2000 2000 2000 2000 2000
- #
- # Alt 70000
- 0 0 0 0 0 0 0 0 0 0 0 0 0
- #
- # THRST3 - THRUST AT FULL AB (THROTL = 1.05)
- #
- # Alt 0
- 27560.8 27285.2 28479.5 31419.3 33991.7 36865 38663.3 36000 35000 35000 35000 35000 35000
- #
- # Alt 10000
- 20670.6 19568.2 20486.9 22967.3 26274.6 29222.3 31919.7 30000 29000 29000 29000 29000 29000
- #
- # Alt 20000
- 13780.4 13596.7 13964.1 15893.4 18373.9 22478.7 25625.7 29042.4 27000 25000 25000 25000 25000
- #
- # Alt 30000
- 8543.85 8268.24 9186.93 10289.4 12953.6 14656.1 19061.9 22478.7 24277 26974.4 29222.3 26000 22000
- #
- # Alt 36000
- 8268.24 7533.29 7717.02 8543.85 9186.93 11688.9 14656.1 17982.9 22119 23377.8 25176.1 27000 22000
- #
- # Alt 40000
- 5971.51 5420.29 5695.9 6522.72 6890.2 8991.47 11958.7 14835.9 17982.9 20140.9 20320.7 23000 18000
- #
- # Alt 50000
- 4409.73 3766.64 4225.99 4474.04 4611.84 5484.79 6923.43 8451.98 9908.6 12318.3 12857.8 11000 9000
- #
- # Alt 70000
- 0 0 0 0 0 0 0 0 0 0 0 0 0
- #
- # ROLL DATA
- #
- #
- # ALPHA BREAKPOINTS
- 7 # Num ALPHA
- -10 0 10 20 30 60 90
- #
- # DYNAMIC PRESSURE BREAKPOINTS
- #
- 7 # Num QBAR
- 0 100 200 300 400 500
- 2000
- #
- # RCMDMX - PEAK ROLL RATE
- #
- 1 # Table Multiplier
- #
- # ALPHA -10
- 0 142.86 200 214.29 242.86 242.86 228.57
- #
- # ALPHA 0
- 0 200 257.14 271.43 300 300 285.71
- #
- # ALPHA 10
- 0 142.86 200 214.29 242.86 242.86 228.57
- #
- # ALPHA 20
- 0 71.43 128.57 142.86 157.14 157.14 142.86
- #
- # ALPHA 30
- 0 7.14 64.29 78.57 107.14 107.14 92.86
- #
- # ALPHA 60
- 0 0 7.14 21.43 50 50 35.71
- #
- # ALPHA 90
- 0
- 0
- 0
- 0
- 0
- 0
- 0
- #
- # End Of Roll Data
- #
- #
- # LIMITERS
- #
- 17 # Number of limiters
- # Type Key Values
- #
- # Neg G Limiter
- 0 0 250 -3 100 0
- # Pos G Limiter (Cat I)
- 3 1 15 9 20.4 7.3 25 1
- # Roll Rate Limiter
- 0 2 15 1 29 1
- # Yaw Alpha Limiter
- 0 3 14 1 26 0
- # Yaw Roll Rate Limiter
- 0 4 20 1 360 0
- # Cat III Command Type
- 0 5 100 7 420 15
- # Cat III AOA Limiter
- 1 6 17
- # Cat III Roll Rate Limiter
- 2 7 0.6
- # Cat III Yaw Alpha Limiter
- 0 8 3 1 15 0
- # Cat III Yaw Roll Rate Limiter
- 0 9 20 1 180 0
- # Pitch and Yaw Control Damper
- 3 10 0 0.3 15 0.85 50 1
- # Roll Control Damper
- 3 11 0 0.6 15 0.85 50 1
- # Command Type
- 1 12 70
- # Low Speed Omega
- 3 13 0.01 0.1 40 0.8 60 1
- # Stores Drag
- 0 14 0.9 0.0001 1 0.000283
- # Cat III Max Gs
- 1 16 6
- # AOA Limiter
- 1 17 26
- #
- # End Of Limiters
- #
- #
- # ADDITIONAL DATA
- #
- normSpoolRate 1.2
- abSpoolRate 1.2
- jfsSpoolUpRate 15
- jfsSpoolUpLimit 0.25
- lightupSpoolRate 10
- flameoutSpoolRate 5
- jfsRechargeTime 60
- jfsMinRechargeRpm 0.12
- jfsSpinTime 240
- mainGenRpm 0.63
- stbyGenRpm 0.6
- epuBurnTime 600
- DeepStallEngineStall 0
- engineDamageStopThreshold 13
- engineDamageNoRestartThreshold 50
- engineDamageHitThreshold 40
- rollMomentum 0.45
- pitchMomentum 0.70
- yawMomentum 1.0
- pitchElasticity 1
- gearPitchFactor 0
- rollGearGain 0.6
- yawGearGain 0.6
- pitchGearGain 0.8
- sinkRate 15
- tefMaxAngle 20
- hasFlapperons 0
- hasTef 0
- CLtefFactor 0.000
- CDtefFactor 0.000
- tefNStages 2
- tefTakeoff 0
- tefRate 20
- lefRate 20
- hasLef 2
- lefGround 2
- lefMaxAngle 20
- lefMaxMach 0.4
- lefNStages 1
- CDlefFactor 0
- CDSPDBFactor 0.03
- CDLDGFactor 0.09
- flapGearRelative 1
- maxFlapVcas 470
- flapVcasRange 250
- area2Span 0.1066
- rudderMaxAngle 20
- aileronMaxAngle 20
- elevonMaxAngle 20
- airbrakeMaxAngle 60
- airbrakeOutRateFactor 1.5
- airbrakeInRateFactor 1.5
- hasSwingWing 0
- isComplex 1
- landingAOA 13
- dragChuteCd 1
- dragChuteMaxSpeed 170
- rollCouple -0.05
- elevatorRoll 1
- canopyMaxAngle 45
- canopyRate 10
- fuelFlowFactorNormal 1.00
- fuelFlowFactorAb 1.95
- minFuelFlow 820
- fuelFwdRes 1312
- fuelAftRes 1312
- fuelFwd1 1020
- fuelAft1 1020
- fuelWingAl 1157
- fuelWingFr 1157
- fuelFwdResRate 22.2
- fuelAftResRate 22.2
- fuelFwd1Rate 22.2
- fuelAft1Rate 22.2
- fuelWingAlRate 6.66
- fuelWingFrRate 6.66
- fuelClineRate 20
- fuelWingExtRate 33.3
- fuelMinFwd 400
- fuelMinAft 400
- nChaff 112
- nFlare 64
- FlareDispensers 3
- FlareSeq 0
- FlarePos1 -13.85 1.65 0.04
- FlareVec1 0 7 40
- FlareCount1 8
- FlarePos2 -13.85 -1.65 0.04
- FlareVec2 0 -7 40
- FlareCount2 8
- FlarePos3 -12.50 0 0.25
- FlareVec3 0 0 45
- FlareCount3 48
- ChaffDispensers 2
- ChaffSeq 2
- ChaffPos1 -16.50 2.50 -0.15
- ChaffVec1 -5 10 2
- ChaffCount1 56
- ChaffPos2 -16.50 -2.50 -0.15
- ChaffVec2 -5 -10 2
- ChaffCount2 56
- gunLocation 7.7 -1.25 4.2
- typeAC 2
- nEngines 1
- engine1Location -22 0 2.1
- engine2Location 0 0 0
- engine3Location 0 0 0
- engine4Location 0 0 0
- engineSmokes 0
- wingTipLocation -10.4 14.8 3.4
- refuelLocation 17 3.5 -0.9
- hardpoint1Grp j10-1/9
- hardpoint2Grp j10-2/8
- hardpoint3Grp j10-3/7
- hardpoint4Grp j10-4/6
- hardpoint5Grp j10-5
- hardpoint6Grp j10-4/6
- hardpoint7Grp j10-3/7
- hardpoint8Grp j10-2/8
- hardpoint9Grp j10-1/9
- hardpoint10Grp 0
- hardpoint11Grp 0
- hardpoint12Grp 0
- hardpoint13Grp 0
- hardpoint14Grp 0
- hardpoint15Grp 0
- hardpoint16Grp 0
- sndSpdBrakeStart 141
- sndSpdBrakeLoop 140
- sndSpdBrakeEnd 139
- sndSpdBrakeWind 142
- sndOverSpeed1 191
- sndOverSpeed2 192
- sndGunStart 25
- sndGunLoop 26
- sndGunEnd 27
- sndBBPullup 68
- sndBBBingo 66
- sndBBWarning 63
- sndBBCaution 64
- sndBBChaffFlareLow 184
- sndBBFlare 138
- sndBBChaffFlare 183
- sndBBChaffFlareOut 185
- sndBBAltitude 65
- sndBBLock 67
- sndTouchDown 42
- sndWheelBrakes 132
- sndDragChute 218
- sndLowSpeed 167
- sndFlapStart 145
- sndFlapLoop 144
- sndFlapEnd 143
- sndHookStart 195
- sndHookLoop 194
- sndHookEnd 193
- sndGearCloseStart 147
- sndGearCloseEnd 146
- sndGearOpenStart 149
- sndGearOpenEnd 150
- sndGearLoop 148
- rollLimitForAiInWP 60
- flap2Nozzle 0
- refuelSpeed 300
- refuelAltitude 22000
- decelDistance 2500
- followRate 60
- desiredClosureFactor 0.45
- IL78Factor 26.4
- longLeg 45
- shortLeg 20
- refuelRate 33
- AIBoomDistance 10
- BingoReturnDistance 50
- jokerFactor 3.1
- bingoFactor 3.1
- fumesFactor 15.4
- maxRippleCount 99
- largePark 0
- Has_TFR 1
- Has_TGP 1
- Has_HTS 1
- PID_K 0.5
- PID_KI 0
- PID_KD 0.39
- TFR_LimitMX 0
- TFR_Corner 420
- TFR_Gain 0.01
- EVA_Gain 5
- TFR_MaxRoll 20
- TFR_SoftG 2
- TFR_MedG 4
- TFR_HardG 6
- TFR_Clearance 20
- SlowPercent 0
- TFR_lookAhead 4000
- EVA1_SoftFactor 0.8
- EVA2_SoftFactor 0.6
- EVA1_MedFactor 0.8
- EVA2_MedFactor 0.6
- EVA1_HardFactor 1.2
- EVA2_HardFactor 0.9
- TFR_GammaCorrMult 1
- LantirnCameraX 10
- LantirnCameraY 2
- LantirnCameraZ 5
- MinTGTMAR 4
- MaxMARIdedStart 20
- AddMARIded5k 0
- AddMARIded18k 2
- AddMARIded28k 4
- AddMARIdedSpike 1
- MaxWEZtaStart 5
- IsShortBurnThreat 0
- IsLongBurnThreat 1
- #Sound Section F-16 PW 200/220/229
- #by Jester
- #Notes - if SndInt is -1 then it defaults to .vcd else use the dat file for whatever index
- #SndWind is not used
- sndWind 33
- sndEject 5
-
- #Engines/Fighters/F-16/SndAbExt.wav
- sndAbExt 39 #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume
- sndAbExtChart 4 0 0 0.7 0.75 0.96 0.97 0.98 1
- sndAbExtPitchChart 3 0.7 2 0.97 1.5 1 1
-
- # engines\fighter\f-16\SndExt.wav - mid range pitch - rear facing
- sndExt 35 #RPM #Volume #RPM #Volume #RPM #Volume
- SndExtChart 3 0 0.8 1 1 1.03 1
- sndExtPitchChart 6 0 0 0.7 1 0.75 1.3 0.8 1.5 0.85 1.7 0.9 1.7 1.03 1.7
-
- # engines\fighter\f-16\SndExt2.wav - near pitch - forward facing
- sndExt2 276 #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume
- SndExt2PitchChart 6 0 0 0.7 1 0.75 1.3 0.83 1.6 0.85 1.8 0.9 1.8 1.03 1.8
- SndExt2Chart 3 0 0.8 1 1 1.03 1
-
- #engines\fighter\f-16\SndInt.wav
- sndInt 34 #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume
- sndIntChart 5 0 0 0.6 1 0.7 1 0.94 1 0.97 0.8
- SndIntPitchChart 6 0 0 0.7 1 0.75 1.3 0.8 1.6 0.85 1.8 0.9 1.8 1.03 1.8
-
- #engines\fighter\f-16\SndInt2.wav
- SndInt2 278 #Pairs #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume
- SndInt2Chart 4 0 0 0.4 0.6 0.7 0.8 0.77 1
- SndInt2PitchChart 6 0 0 0.7 1 0.75 1 0.83 1.008 0.85 1.01 0.9 1.012 1.03 1.012
-
- #engines\fighter\f-16\SndInt3.wav
- SndInt3 303 #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume
- SndInt3Chart 5 0 0 0.3 1 0.7 1 0.8 1 0.94 1
- SndInt3PitchChart 6 0 0 0.7 1 0.75 1 0.83 1.008 0.85 1.01 0.9 1.012 1.03 1.012
-
- #engines\fighter\f-16\SndAbInt.wav
- sndAbInt 40 #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume
- SndAbIntChart 3 0 0 0.9 0.2 0.97 1
-
- #engines\fighter\f-16\SndAbInt2.wav
- SndAbInt2 297 #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume
- SndAbInt2Chart 2 0 0 0.93 1
-
- SndAero1 298
- #The will increase the sound level at high speed and at any AOA.
- sndAero1AOAChart 1 0 1 1 0 1
- sndAero1SpeedChart 2 0 0 0.97 1
- #higher speed lower AoA (more G)
- SndAero2 299
- sndAero2AOAChart 3 0 0 8 0 15 1 20 1
- sndAero2SpeedChart 2 0 0 .8 1
-
- SndAero3 300
- sndAero2AOAChart 3 0 0 5 .75 6 1 12 1
- sndAero3SpeedChart 2 0 0 .86 1
- PilotEyePos 12 0 -1.6
- # animStrobeOnTime 0.02
- # animStrobeOffTime 1.0
- # animWingFlashOnTime 0.4
- # animWingFlashOffTime 0.25
- animWheelRadius1 0.75
- animWheelRadius2 1.1
- animWheelRadius3 1.1
- animGearMaxComp1 0.25
- animGearMaxComp2 0.0
- animGearMaxComp3 0.0
- animGearMaxExt1 0.5
- animGearMaxExt2 0.15
- animGearMaxExt3 0.15
- # animExhNozIdle 5.0
- # animExhNozMil 21.0
- # animExhNozAB 15.0
- # animExhNozRate 50.0
- A2GHarmAlt 20000.0
- A2GAGMAlt 8000.0
- A2GGBUAlt 20000.0
- A2GDumbHDAlt 1500
- A2GClusterAlt 14000.0
- A2GDumbLDAlt 16000.0
- A2GGunRocketAlt 3500.0
- A2GCameraAlt 12000.0
- FlareDispensers 2
- FlareSeq 0
- FlarePos1 -7.5 -3 1
- FlareVec1 0 0 200
- FlareCount1 15
- FlarePos2 -8.5 -3 1
- FlareVec2 0 0 200
- FlareCount2 15
- ChaffDispensers 2
- ChaffSeq 0
- ChaffPos1 -10 -3 1
- ChaffVec1 0 -8 100
- ChaffCount1 30
- ChaffPos2 -10 -3 1
- ChaffVec2 0 -8 100
- ChaffCount2 30
- sndCanopyOpenStart 271
- sndCanopyOpenEnd 272
- sndCanopyCloseStart 273
- sndCanopyCloseEnd 274
- sndCanopyLoop 275
- hasEWS 1
- # left wing looking towards cockpit
- TopGunCamera1 7 -4.72 -15.63 -4.4 0.0 45.0 0.0 60.0
- # right of cockpit looking toward pilots
- TopGunCamera2 7 19.38 -8.16 -3.77 -5.0 135.0 0.0 65.0
- # before air intake looking backwards to gear..
- TopGunCamera3 7 19.0 -0.0 3.08 -2.0 -180.0 0.0 60.0
- # placed near the gun, looking forward..
- #TopGunCamera4 7 0.0 0.0 -25.0 -90.0 90.0 0.0 95.0
- TopGunCamera4 7 43.0 0.0 -9.0 -16.0 180.0 0.0 47.0
- complexnozzle 1
- AFMcriticalAOA 26
- pitchElevatorTrimRate 0.15
- pitchAileronTrimRate 0.04
- pitchRudderTrimRate 0.25
- Light1Position -4.9 15 -2
- Light1Color 0 .4 0
- Light1Type 3
- Light1Radius 25
- Light1Attenuation .7
- Light2Position -4.9 15 1
- Light2Color 0 .4 0
- Light2Type 3
- Light2Radius 25
- Light2Attenuation .7
- Light3Position 12.4 2.7 1.3
- Light3Color 0 .4 0
- Light3Type 3
- Light3Radius 25
- Light3Attenuation .7
- Light4Position -4.9 -15 -2
- Light4Color .4 0 0
- Light4Type 3
- Light4Radius 25
- Light4Attenuation .7
- Light5Position -4.9 -15 1
- Light5Color .4 0 0
- Light5Type 3
- Light5Radius 25
- Light5Attenuation .7
- Light6Position 12.4 -2.7 1.3
- Light6Color .4 0 0
- Light6Type 3
- Light6Radius 25
- Light6Attenuation .7
- Light7Position -18.00 -1.5 -11.24
- Light7Color .2 .2 .5
- Light7Type 1
- Light7Radius 28
- Light7Attenuation .1
- Light8Position -18.00 1.5 -11.24
- Light8Color .2 .2 .5
- Light8Type 1
- Light8Radius 28
- Light8Attenuation .1
- SpotLight1Color 0.25 0.25 0.24 # color of the light
- SpotLight1LookAt 12.34 0.58 4.23 # position in model space at which the light should point
- SpotLight1Position 11.54 0.58 3.73 # the light's position
- SpotLight1Attenuation 0.0001 # attenuation of the light
- SpotLight1InnerConeDeg 30 # inner cone angle in degrees
- SpotLight1OuterConeDeg 45 # outer cone angle in degrees
- HasOldLandingLight 1
- AFMcriticalAOA 25
- #
- #JetBlast data
- Wakefactor 1
- # 1 is default
- WakeAngle 4.28
- # 2 degree is default
- WakeDistance 668
- # 800 is default
- #
- # End of Additional
- #
- END OF DATA
biller 发表于 2014-12-12 13:07
....这外模怎么样?
外模比较一般、舱内有一部分仿照F16(不仿就不能冷启)、气动一塌糊涂。
顺道补一下从FreeFalcon转过来的歼十OFM
- #
- #A-G Weapons release profile added April 19, 2004 JimG
- #Renard modified from Free Falcon J10.dat
- #
- # SIMULATION INPUT PANEL
- #
- # INPUT MASS AND GEOMETRIC PROPERTIES:
- 19884 # Empty Weight (lbs)
- 437 # Reference Area
- 7900 # Internal Fuel
- #
- #
- # ANGLE OF ATTACK AND SIDESLIP LIMITS
- 35 # AOA Max
- -15 # AOA Min
- 15 # Beta Max
- -15 # Beta Min
- 9 # Max G
- 190 # Max Roll
- 250 # Min Vcas
- 900 # Max Vcas
- 420 # Corner Vcas
- 12 # Theta Max
- 3 # Num Gear
- # Gear X. Y. Z. Rng
- 15.9 0 8.2 100
- 28.6 -2.6 7.3 100
- 28.6 2.6 7.3 100
- #
- # Physical data
- 25.77 # CG Loc
- 46.85 # Length
- 27.16 # Span
- 3 # Fus Radius
- 13.6 # Tail Ht
- #
- # End of Airframe data
- #
- #
- #
- # BASIC AERODYNAMIC COEFFICIENTS
- #
- #
- # MACH BREAKPOINTS
- #
- 10 # Num MACH
- 0 0.2 0.4 0.69
- 0.83 0.89 0.95 1.2 1.6
- 2.5
- #
- # ALPHA BREAKPOINTS
- #
- 12 # Num Alpha
- -20 -10 -5 0
- 5 10 15 20 25
- 30 35 40
- #
- # LIFT COEFFICIENT CL
- #
- 1 # Table Multiplier
- #
- # Mach 0.000
- -1.09716 -0.83076 -0.36744 -0.06 0.198 0.42 0.654 0.83456 1.04864 1.252 1.348 1.336
- #
- # Mach 0.200
- -1.09716 -0.83076 -0.36744 -0.06 0.198 0.42 0.654 0.83456 1.04864 1.252 1.348 1.336
- #
- # Mach 0.400
- -1.09716 -0.83076 -0.36744 -0.06 0.198 0.42 0.654 0.93456 1.14864 1.452 1.548 1.536
- #
- # Mach 0.690
- -1.09716 -0.83076 -0.36744 -0.06 0.198 0.42 0.654 0.93456 1.14864 1.452 1.548 1.536
- #
- # Mach 0.830
- -0.939 -0.714 -0.3246 -0.06 0.173 0.374 0.575 0.80492 0.97162 1.22852 1.33182 1.32792
- #
- # Mach 0.890
- -0.97 -0.7244 -0.3434 -0.06 0.18 0.375 0.575 0.84088 1.00698 1.26258 1.36808 1.37248
- #
- # Mach 0.950
- -1.0322 -0.7444 -0.3634 -0.08 0.175 0.385 0.68104 0.95714 1.12324 1.37884 1.48434 1.48874
- #
- # Mach 1.200
- -1.0322 -0.7634 -0.3866 -0.1 0.15 0.40804 0.74834 1.02474 1.19674 1.45524 1.55414 1.56414
- #
- # Mach 1.600
- -1.0322 -0.7634 -0.3866 -0.1 0.15 0.40804 0.74834 1.02474 1.19674 1.45524 1.55414 1.56414
- #
- # Mach 2.500
- -1.0322 -0.7634 -0.386 -0.1 0.15 0.40804 0.74834 1.02474 1.19674 1.45524 1.55414 1.56414
- #
- # DRAG COEFFICIENT CD
- #
- 0.66666 # Table Multiplier
- #
- # Mach 0.000
- 0.2381 0.1882 0.0759 0.0223 0.0259 0.0353 0.0827333 0.176667 0.349733 0.5784 0.669127 0.878
- #
- # Mach 0.200
- 0.1945 0.15461 0.0647079 0.0228899 0.02595 0.0353 0.0827333 0.183333 0.359783 0.580913 0.67794 0.947713
- #
- # Mach 0.400
- 0.1945 0.15461 0.0647079 0.0228899 0.02595 0.0353 0.0827333 0.183333 0.359783 0.580913 0.67794 0.947713
- #
- # Mach 0.690
- 0.2046 0.164864 0.0706953 0.0235326 0.0243 0.0415 0.09805 0.21246 0.38537 0.614628 0.804227 1.01579
- #
- # Mach 0.830
- 0.2048 0.165003 0.0708347 0.0236719 0.02446 0.04558 0.11275 0.242707 0.413821 0.643079 0.83268 1.04424
- #
- # Mach 0.890
- 0.2077 0.161755 0.0738287 0.024244 0.0246 0.0485 0.11225 0.262248 0.429649 0.663252 0.933667 1.05351
- #
- # Mach 0.950
- 0.2076 0.16167 0.073742 0.0243388 0.0245 0.0495 0.16208 0.325518 0.492919 0.72652 0.99694 1.11678
- #
- # Mach 1.200
- 0.2198 0.150914 0.0805253 0.0210382 0.0355 0.04402 0.147503 0.312995 0.46 0.778927 1.03939 1.1747
- #
- # Mach 1.600
- 0.2198 0.150914 0.0805253 0.0203715 0.038 0.045228 0.128933 0.2662 0.394767 0.907927 1.16839 1.30372
- #
- # Mach 2.500
- 0.2188 0.149914 0.0795253 0.0200382 0.0375 0.0366853 0.12 0.259684 0.391267 0.92562 1.18608 1.32141
- #
- # SIDE FORCE DERIVATIVE CY-BETA
- #
- 1 # Table Multiplier
- #
- # Mach 0.00
- -0.0109 -0.0166 -0.0182 -0.0192 -0.0187 -0.0163
- -0.0176 -0.0164 -0.0158 -0.0141 -0.009 -0.011
- #
- # Mach 0.20
- -0.0109 -0.0166 -0.0182 -0.0192 -0.0187 -0.0163
- -0.0176 -0.0164 -0.0158 -0.0141 -0.009 -0.016
- #
- # Mach 0.40
- -0.0109 -0.0166 -0.0182 -0.0192 -0.0187 -0.0163
- -0.0176 -0.0164 -0.0158 -0.0141 -0.009 -0.016
- #
- # Mach 0.69
- -0.0122 -0.021 -0.028 -0.0286 -0.03 -0.025
- -0.0267 -0.0223 -0.0215 -0.0187 -0.0172 -0.017
- #
- # Mach 0.83
- -0.0172 -0.027 -0.033 -0.035 -0.0333 -0.0321
- -0.0288 -0.0254 -0.0231 -0.0207 -0.0188 -0.0171
- #
- # Mach 0.89
- -0.01725 -0.0271 -0.03325 -0.03525 -0.03355 -0.03235
- -0.029 -0.0257 -0.02355 -0.02085 -0.0194 -0.01715
- #
- # Mach 0.95
- -0.017275 -0.02715 -0.033375 -0.035375 -0.033675 -0.032475
- -0.0291 -0.02585 -0.023775 -0.020925 -0.0197 -0.0172
- #
- # Mach 1.20
- -0.0173 -0.0272 -0.0335 -0.0355 -0.0338 -0.0326
- -0.0292 -0.026 -0.024 -0.021 -0.02 -0.0172
- #
- # Mach 1.60
- -0.0173 -0.0272 -0.0335 -0.0355 -0.0338 -0.0326
- -0.0292 -0.026 -0.024 -0.021 -0.02 -0.0161
- #
- # Mach 2.50
- -0.0162 -0.0194 -0.0194 -0.0215 -0.0216 -0.0214
- -0.0215 -0.0205 -0.0179 -0.0153 -0.0105 -0.0161
- # End of Aero Data
- #
- #
- # PROPULSION DATA
- #
- 1 # Thrust multiplier
- 0.6 # Fuel Flow Multiplier
- #
- # MACH BREAKPOINTS
- #
- 13 # Number of Mach Breaks
- 0 0.2 0.4 0.6 0.8 1
- 1.2 1.4 1.6 1.8 2 2.4 2.5
- #
- # ALTITUDE BREAKPOINTS
- #
- 8 # Number of Alt Break Points
- 0 10000 20000 30000 36000 40000
- 50000 70000
- #
- # THRST1 - THRUST AT IDLE (THROTL = 0.00)
- #
- # Alt 0
- 0 -800 -1700 -2200 -3300 -4000 -4900 -5900 -6700 -7700 -8600 -10800 -10800
- #
- # Alt 10000
- 0 -400 -1100 -1650 -2250 -2800 -3450 -4050 -4600 -5100 -5750 -7400 -7400
- #
- # Alt 20000
- 0 -370 -740 -1100 -1480 -1850 -2230 -2550 -2900 -3330 -3700 -4625 -4625
- #
- # Alt 30000
- 0 -230 -450 -690 -920 -1150 -1380 -1600 -1850 -2075 -2300 -2880 -2880
- #
- # Alt 36000
- 0 -160 -340 -500 -675 -850 -1000 -1190 -1360 -1520 -1700 -2125 -2125
- #
- # Alt 40000
- 0 -140 -275 -415 -550 -690 -835 -975 -1115 -1250 -1390 -1740 -1740
- #
- # Alt 50000
- 0 -80 -170 -255 -345 -430 -515 -600 -690 -775 -860 -1075 -1075
- #
- # Alt 70000
- 0 -40 -85 -125 -165 -210 -250 -290 -335 -375 -420 -525 -525
- #
- # THRST2 - THRUST AT MIL POWER (THROTL = 1.00)
- #
- # Alt 0
- 16779 15520.6 16107.8 17198.5 18037.4 18474.8 18000 18000 18000 18000 18000 18000 18000
- #
- # Alt 10000
- 12500.4 11325.8 11158 12584.3 14262.2 14861.9 12000 10000 10000 10000 10000 10000 10000
- #
- # Alt 20000
- 8389.5 7298.87 6711.6 8389.5 9647.92 11495.4 10900 10300 10000 10000 10000 10000 10000
- #
- # Alt 30000
- 5872.65 5453.17 5033.7 5285.38 6292.13 6979.35 7100 6600 6600 6600 6600 6000 6000
- #
- # Alt 36000
- 4194.75 4152.8 4068.91 4194.75 4614.23 5994.03 6100 5500 5500 5000 5000 5000 5000
- #
- # Alt 40000
- 3355.8 3271.91 2936.32 3188.01 4110.85 4598.16 4444 4000 4000 4000 4000 4000 4000
- #
- # Alt 50000
- 2097.38 2013.48 1988.31 2105.76 2516.85 2700 2200 2000 2000 2000 2000 2000 2000
- #
- # Alt 70000
- 0 0 0 0 0 0 0 0 0 0 0 0 0
- #
- # THRST3 - THRUST AT FULL AB (THROTL = 1.05)
- #
- # Alt 0
- 27560.8 27285.2 28479.5 31419.3 33991.7 36865 38663.3 36000 35000 35000 35000 35000 35000
- #
- # Alt 10000
- 20670.6 19568.2 20486.9 22967.3 26274.6 29222.3 31919.7 30000 29000 29000 29000 29000 29000
- #
- # Alt 20000
- 13780.4 13596.7 13964.1 15893.4 18373.9 22478.7 25625.7 29042.4 27000 25000 25000 25000 25000
- #
- # Alt 30000
- 8543.85 8268.24 9186.93 10289.4 12953.6 14656.1 19061.9 22478.7 24277 26974.4 29222.3 26000 22000
- #
- # Alt 36000
- 8268.24 7533.29 7717.02 8543.85 9186.93 11688.9 14656.1 17982.9 22119 23377.8 25176.1 27000 22000
- #
- # Alt 40000
- 5971.51 5420.29 5695.9 6522.72 6890.2 8991.47 11958.7 14835.9 17982.9 20140.9 20320.7 23000 18000
- #
- # Alt 50000
- 4409.73 3766.64 4225.99 4474.04 4611.84 5484.79 6923.43 8451.98 9908.6 12318.3 12857.8 11000 9000
- #
- # Alt 70000
- 0 0 0 0 0 0 0 0 0 0 0 0 0
- #
- # ROLL DATA
- #
- #
- # ALPHA BREAKPOINTS
- 7 # Num ALPHA
- -10 0 10 20 30 60 90
- #
- # DYNAMIC PRESSURE BREAKPOINTS
- #
- 7 # Num QBAR
- 0 100 200 300 400 500
- 2000
- #
- # RCMDMX - PEAK ROLL RATE
- #
- 1 # Table Multiplier
- #
- # ALPHA -10
- 0 142.86 200 214.29 242.86 242.86 228.57
- #
- # ALPHA 0
- 0 200 257.14 271.43 300 300 285.71
- #
- # ALPHA 10
- 0 142.86 200 214.29 242.86 242.86 228.57
- #
- # ALPHA 20
- 0 71.43 128.57 142.86 157.14 157.14 142.86
- #
- # ALPHA 30
- 0 7.14 64.29 78.57 107.14 107.14 92.86
- #
- # ALPHA 60
- 0 0 7.14 21.43 50 50 35.71
- #
- # ALPHA 90
- 0
- 0
- 0
- 0
- 0
- 0
- 0
- #
- # End Of Roll Data
- #
- #
- # LIMITERS
- #
- 17 # Number of limiters
- # Type Key Values
- #
- # Neg G Limiter
- 0 0 250 -3 100 0
- # Pos G Limiter (Cat I)
- 3 1 15 9 20.4 7.3 25 1
- # Roll Rate Limiter
- 0 2 15 1 29 1
- # Yaw Alpha Limiter
- 0 3 14 1 26 0
- # Yaw Roll Rate Limiter
- 0 4 20 1 360 0
- # Cat III Command Type
- 0 5 100 7 420 15
- # Cat III AOA Limiter
- 1 6 17
- # Cat III Roll Rate Limiter
- 2 7 0.6
- # Cat III Yaw Alpha Limiter
- 0 8 3 1 15 0
- # Cat III Yaw Roll Rate Limiter
- 0 9 20 1 180 0
- # Pitch and Yaw Control Damper
- 3 10 0 0.3 15 0.85 50 1
- # Roll Control Damper
- 3 11 0 0.6 15 0.85 50 1
- # Command Type
- 1 12 70
- # Low Speed Omega
- 3 13 0.01 0.1 40 0.8 60 1
- # Stores Drag
- 0 14 0.9 0.0001 1 0.000283
- # Cat III Max Gs
- 1 16 6
- # AOA Limiter
- 1 17 26
- #
- # End Of Limiters
- #
- #
- # ADDITIONAL DATA
- #
- normSpoolRate 1.2
- abSpoolRate 1.2
- jfsSpoolUpRate 15
- jfsSpoolUpLimit 0.25
- lightupSpoolRate 10
- flameoutSpoolRate 5
- jfsRechargeTime 60
- jfsMinRechargeRpm 0.12
- jfsSpinTime 240
- mainGenRpm 0.63
- stbyGenRpm 0.6
- epuBurnTime 600
- DeepStallEngineStall 0
- engineDamageStopThreshold 13
- engineDamageNoRestartThreshold 50
- engineDamageHitThreshold 40
- rollMomentum 0.45
- pitchMomentum 0.70
- yawMomentum 1.0
- pitchElasticity 1
- gearPitchFactor 0
- rollGearGain 0.6
- yawGearGain 0.6
- pitchGearGain 0.8
- sinkRate 15
- tefMaxAngle 20
- hasFlapperons 0
- hasTef 0
- CLtefFactor 0.000
- CDtefFactor 0.000
- tefNStages 2
- tefTakeoff 0
- tefRate 20
- lefRate 20
- hasLef 2
- lefGround 2
- lefMaxAngle 20
- lefMaxMach 0.4
- lefNStages 1
- CDlefFactor 0
- CDSPDBFactor 0.03
- CDLDGFactor 0.09
- flapGearRelative 1
- maxFlapVcas 470
- flapVcasRange 250
- area2Span 0.1066
- rudderMaxAngle 20
- aileronMaxAngle 20
- elevonMaxAngle 20
- airbrakeMaxAngle 60
- airbrakeOutRateFactor 1.5
- airbrakeInRateFactor 1.5
- hasSwingWing 0
- isComplex 1
- landingAOA 13
- dragChuteCd 1
- dragChuteMaxSpeed 170
- rollCouple -0.05
- elevatorRoll 1
- canopyMaxAngle 45
- canopyRate 10
- fuelFlowFactorNormal 1.00
- fuelFlowFactorAb 1.95
- minFuelFlow 820
- fuelFwdRes 1312
- fuelAftRes 1312
- fuelFwd1 1020
- fuelAft1 1020
- fuelWingAl 1157
- fuelWingFr 1157
- fuelFwdResRate 22.2
- fuelAftResRate 22.2
- fuelFwd1Rate 22.2
- fuelAft1Rate 22.2
- fuelWingAlRate 6.66
- fuelWingFrRate 6.66
- fuelClineRate 20
- fuelWingExtRate 33.3
- fuelMinFwd 400
- fuelMinAft 400
- nChaff 112
- nFlare 64
- FlareDispensers 3
- FlareSeq 0
- FlarePos1 -13.85 1.65 0.04
- FlareVec1 0 7 40
- FlareCount1 8
- FlarePos2 -13.85 -1.65 0.04
- FlareVec2 0 -7 40
- FlareCount2 8
- FlarePos3 -12.50 0 0.25
- FlareVec3 0 0 45
- FlareCount3 48
- ChaffDispensers 2
- ChaffSeq 2
- ChaffPos1 -16.50 2.50 -0.15
- ChaffVec1 -5 10 2
- ChaffCount1 56
- ChaffPos2 -16.50 -2.50 -0.15
- ChaffVec2 -5 -10 2
- ChaffCount2 56
- gunLocation 7.7 -1.25 4.2
- typeAC 2
- nEngines 1
- engine1Location -22 0 2.1
- engine2Location 0 0 0
- engine3Location 0 0 0
- engine4Location 0 0 0
- engineSmokes 0
- wingTipLocation -10.4 14.8 3.4
- refuelLocation 17 3.5 -0.9
- hardpoint1Grp j10-1/9
- hardpoint2Grp j10-2/8
- hardpoint3Grp j10-3/7
- hardpoint4Grp j10-4/6
- hardpoint5Grp j10-5
- hardpoint6Grp j10-4/6
- hardpoint7Grp j10-3/7
- hardpoint8Grp j10-2/8
- hardpoint9Grp j10-1/9
- hardpoint10Grp 0
- hardpoint11Grp 0
- hardpoint12Grp 0
- hardpoint13Grp 0
- hardpoint14Grp 0
- hardpoint15Grp 0
- hardpoint16Grp 0
- sndSpdBrakeStart 141
- sndSpdBrakeLoop 140
- sndSpdBrakeEnd 139
- sndSpdBrakeWind 142
- sndOverSpeed1 191
- sndOverSpeed2 192
- sndGunStart 25
- sndGunLoop 26
- sndGunEnd 27
- sndBBPullup 68
- sndBBBingo 66
- sndBBWarning 63
- sndBBCaution 64
- sndBBChaffFlareLow 184
- sndBBFlare 138
- sndBBChaffFlare 183
- sndBBChaffFlareOut 185
- sndBBAltitude 65
- sndBBLock 67
- sndTouchDown 42
- sndWheelBrakes 132
- sndDragChute 218
- sndLowSpeed 167
- sndFlapStart 145
- sndFlapLoop 144
- sndFlapEnd 143
- sndHookStart 195
- sndHookLoop 194
- sndHookEnd 193
- sndGearCloseStart 147
- sndGearCloseEnd 146
- sndGearOpenStart 149
- sndGearOpenEnd 150
- sndGearLoop 148
- rollLimitForAiInWP 60
- flap2Nozzle 0
- refuelSpeed 300
- refuelAltitude 22000
- decelDistance 2500
- followRate 60
- desiredClosureFactor 0.45
- IL78Factor 26.4
- longLeg 45
- shortLeg 20
- refuelRate 33
- AIBoomDistance 10
- BingoReturnDistance 50
- jokerFactor 3.1
- bingoFactor 3.1
- fumesFactor 15.4
- maxRippleCount 99
- largePark 0
- Has_TFR 1
- Has_TGP 1
- Has_HTS 1
- PID_K 0.5
- PID_KI 0
- PID_KD 0.39
- TFR_LimitMX 0
- TFR_Corner 420
- TFR_Gain 0.01
- EVA_Gain 5
- TFR_MaxRoll 20
- TFR_SoftG 2
- TFR_MedG 4
- TFR_HardG 6
- TFR_Clearance 20
- SlowPercent 0
- TFR_lookAhead 4000
- EVA1_SoftFactor 0.8
- EVA2_SoftFactor 0.6
- EVA1_MedFactor 0.8
- EVA2_MedFactor 0.6
- EVA1_HardFactor 1.2
- EVA2_HardFactor 0.9
- TFR_GammaCorrMult 1
- LantirnCameraX 10
- LantirnCameraY 2
- LantirnCameraZ 5
- MinTGTMAR 4
- MaxMARIdedStart 20
- AddMARIded5k 0
- AddMARIded18k 2
- AddMARIded28k 4
- AddMARIdedSpike 1
- MaxWEZtaStart 5
- IsShortBurnThreat 0
- IsLongBurnThreat 1
- #Sound Section F-16 PW 200/220/229
- #by Jester
- #Notes - if SndInt is -1 then it defaults to .vcd else use the dat file for whatever index
- #SndWind is not used
- sndWind 33
- sndEject 5
-
- #Engines/Fighters/F-16/SndAbExt.wav
- sndAbExt 39 #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume
- sndAbExtChart 4 0 0 0.7 0.75 0.96 0.97 0.98 1
- sndAbExtPitchChart 3 0.7 2 0.97 1.5 1 1
-
- # engines\fighter\f-16\SndExt.wav - mid range pitch - rear facing
- sndExt 35 #RPM #Volume #RPM #Volume #RPM #Volume
- SndExtChart 3 0 0.8 1 1 1.03 1
- sndExtPitchChart 6 0 0 0.7 1 0.75 1.3 0.8 1.5 0.85 1.7 0.9 1.7 1.03 1.7
-
- # engines\fighter\f-16\SndExt2.wav - near pitch - forward facing
- sndExt2 276 #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume
- SndExt2PitchChart 6 0 0 0.7 1 0.75 1.3 0.83 1.6 0.85 1.8 0.9 1.8 1.03 1.8
- SndExt2Chart 3 0 0.8 1 1 1.03 1
-
- #engines\fighter\f-16\SndInt.wav
- sndInt 34 #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume
- sndIntChart 5 0 0 0.6 1 0.7 1 0.94 1 0.97 0.8
- SndIntPitchChart 6 0 0 0.7 1 0.75 1.3 0.8 1.6 0.85 1.8 0.9 1.8 1.03 1.8
-
- #engines\fighter\f-16\SndInt2.wav
- SndInt2 278 #Pairs #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume
- SndInt2Chart 4 0 0 0.4 0.6 0.7 0.8 0.77 1
- SndInt2PitchChart 6 0 0 0.7 1 0.75 1 0.83 1.008 0.85 1.01 0.9 1.012 1.03 1.012
-
- #engines\fighter\f-16\SndInt3.wav
- SndInt3 303 #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume
- SndInt3Chart 5 0 0 0.3 1 0.7 1 0.8 1 0.94 1
- SndInt3PitchChart 6 0 0 0.7 1 0.75 1 0.83 1.008 0.85 1.01 0.9 1.012 1.03 1.012
-
- #engines\fighter\f-16\SndAbInt.wav
- sndAbInt 40 #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume
- SndAbIntChart 3 0 0 0.9 0.2 0.97 1
-
- #engines\fighter\f-16\SndAbInt2.wav
- SndAbInt2 297 #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume #RPM #Volume
- SndAbInt2Chart 2 0 0 0.93 1
-
- SndAero1 298
- #The will increase the sound level at high speed and at any AOA.
- sndAero1AOAChart 1 0 1 1 0 1
- sndAero1SpeedChart 2 0 0 0.97 1
- #higher speed lower AoA (more G)
- SndAero2 299
- sndAero2AOAChart 3 0 0 8 0 15 1 20 1
- sndAero2SpeedChart 2 0 0 .8 1
-
- SndAero3 300
- sndAero2AOAChart 3 0 0 5 .75 6 1 12 1
- sndAero3SpeedChart 2 0 0 .86 1
- PilotEyePos 12 0 -1.6
- # animStrobeOnTime 0.02
- # animStrobeOffTime 1.0
- # animWingFlashOnTime 0.4
- # animWingFlashOffTime 0.25
- animWheelRadius1 0.75
- animWheelRadius2 1.1
- animWheelRadius3 1.1
- animGearMaxComp1 0.25
- animGearMaxComp2 0.0
- animGearMaxComp3 0.0
- animGearMaxExt1 0.5
- animGearMaxExt2 0.15
- animGearMaxExt3 0.15
- # animExhNozIdle 5.0
- # animExhNozMil 21.0
- # animExhNozAB 15.0
- # animExhNozRate 50.0
- A2GHarmAlt 20000.0
- A2GAGMAlt 8000.0
- A2GGBUAlt 20000.0
- A2GDumbHDAlt 1500
- A2GClusterAlt 14000.0
- A2GDumbLDAlt 16000.0
- A2GGunRocketAlt 3500.0
- A2GCameraAlt 12000.0
- FlareDispensers 2
- FlareSeq 0
- FlarePos1 -7.5 -3 1
- FlareVec1 0 0 200
- FlareCount1 15
- FlarePos2 -8.5 -3 1
- FlareVec2 0 0 200
- FlareCount2 15
- ChaffDispensers 2
- ChaffSeq 0
- ChaffPos1 -10 -3 1
- ChaffVec1 0 -8 100
- ChaffCount1 30
- ChaffPos2 -10 -3 1
- ChaffVec2 0 -8 100
- ChaffCount2 30
- sndCanopyOpenStart 271
- sndCanopyOpenEnd 272
- sndCanopyCloseStart 273
- sndCanopyCloseEnd 274
- sndCanopyLoop 275
- hasEWS 1
- # left wing looking towards cockpit
- TopGunCamera1 7 -4.72 -15.63 -4.4 0.0 45.0 0.0 60.0
- # right of cockpit looking toward pilots
- TopGunCamera2 7 19.38 -8.16 -3.77 -5.0 135.0 0.0 65.0
- # before air intake looking backwards to gear..
- TopGunCamera3 7 19.0 -0.0 3.08 -2.0 -180.0 0.0 60.0
- # placed near the gun, looking forward..
- #TopGunCamera4 7 0.0 0.0 -25.0 -90.0 90.0 0.0 95.0
- TopGunCamera4 7 43.0 0.0 -9.0 -16.0 180.0 0.0 47.0
- complexnozzle 1
- AFMcriticalAOA 26
- pitchElevatorTrimRate 0.15
- pitchAileronTrimRate 0.04
- pitchRudderTrimRate 0.25
- Light1Position -4.9 15 -2
- Light1Color 0 .4 0
- Light1Type 3
- Light1Radius 25
- Light1Attenuation .7
- Light2Position -4.9 15 1
- Light2Color 0 .4 0
- Light2Type 3
- Light2Radius 25
- Light2Attenuation .7
- Light3Position 12.4 2.7 1.3
- Light3Color 0 .4 0
- Light3Type 3
- Light3Radius 25
- Light3Attenuation .7
- Light4Position -4.9 -15 -2
- Light4Color .4 0 0
- Light4Type 3
- Light4Radius 25
- Light4Attenuation .7
- Light5Position -4.9 -15 1
- Light5Color .4 0 0
- Light5Type 3
- Light5Radius 25
- Light5Attenuation .7
- Light6Position 12.4 -2.7 1.3
- Light6Color .4 0 0
- Light6Type 3
- Light6Radius 25
- Light6Attenuation .7
- Light7Position -18.00 -1.5 -11.24
- Light7Color .2 .2 .5
- Light7Type 1
- Light7Radius 28
- Light7Attenuation .1
- Light8Position -18.00 1.5 -11.24
- Light8Color .2 .2 .5
- Light8Type 1
- Light8Radius 28
- Light8Attenuation .1
- SpotLight1Color 0.25 0.25 0.24 # color of the light
- SpotLight1LookAt 12.34 0.58 4.23 # position in model space at which the light should point
- SpotLight1Position 11.54 0.58 3.73 # the light's position
- SpotLight1Attenuation 0.0001 # attenuation of the light
- SpotLight1InnerConeDeg 30 # inner cone angle in degrees
- SpotLight1OuterConeDeg 45 # outer cone angle in degrees
- HasOldLandingLight 1
- AFMcriticalAOA 25
- #
- #JetBlast data
- Wakefactor 1
- # 1 is default
- WakeAngle 4.28
- # 2 degree is default
- WakeDistance 668
- # 800 is default
- #
- # End of Additional
- #
- END OF DATA
怎么搞进BMS4里?求支招
这MOD要能做好,搞不好飞BMS的人能变多。。。。
反正BearStudio's J-10 for FSX 感觉就这样。。。
反正BearStudio's J-10 for FSX 感觉就这样。。。
biller 发表于 2015-1-6 18:32
这MOD要能做好,搞不好飞BMS的人能变多。。。。
反正BearStudio's J-10 for FSX 感觉就这样。。。
其实目前只能算个壳子机,对于鸭翼特性模拟的太烂
这MOD要能做好,搞不好飞BMS的人能变多。。。。
反正BearStudio's J-10 for FSX 感觉就这样。。。
其实目前只能算个壳子机,对于鸭翼特性模拟的太烂
biller 发表于 2015-1-6 18:32
这MOD要能做好,搞不好飞BMS的人能变多。。。。
反正BearStudio's J-10 for FSX 感觉就这样。。。
这个MOD所有素材都是由bear studio提供的。Falcon BMS没有鸭翼,只能用平尾移位来替换。
biller 发表于 2015-1-6 18:32
这MOD要能做好,搞不好飞BMS的人能变多。。。。
反正BearStudio's J-10 for FSX 感觉就这样。。。
这个MOD所有素材都是由bear studio提供的。Falcon BMS没有鸭翼,只能用平尾移位来替换。
雷纳尔 发表于 2015-1-8 23:27
这个MOD所有素材都是由bear studio提供的。Falcon BMS没有鸭翼,只能用平尾移位来替换。
.........我觉得MOD应该去找skierider或者rick。。。。或者mikezj。。。他们都有比这个质量高的机模。。。
这个MOD所有素材都是由bear studio提供的。Falcon BMS没有鸭翼,只能用平尾移位来替换。
.........我觉得MOD应该去找skierider或者rick。。。。或者mikezj。。。他们都有比这个质量高的机模。。。
这OFM也太搞笑了
biller 发表于 2015-1-9 18:00
.........我觉得MOD应该去找skierider或者rick。。。。或者mikezj。。。他们都有比这个质量高的机模。。 ...
FC 系列还是算了吧 ,熊也是本土选手。
biller 发表于 2015-1-9 18:00
.........我觉得MOD应该去找skierider或者rick。。。。或者mikezj。。。他们都有比这个质量高的机模。。 ...
FC 系列还是算了吧 ,熊也是本土选手。
孔经纬 发表于 2015-1-9 19:40
这OFM也太搞笑了
好像还没有那款模拟飞行游戏的鸭翼机FM不搞笑。
这OFM也太搞笑了
好像还没有那款模拟飞行游戏的鸭翼机FM不搞笑。
雷纳尔 发表于 2015-1-9 21:25
FC 系列还是算了吧 ,熊也是本土选手。
外模的质量 F4系列的就从没超过FC里面的,尤其是歼10的机模
FC 系列还是算了吧 ,熊也是本土选手。
外模的质量 F4系列的就从没超过FC里面的,尤其是歼10的机模
biller 发表于 2015-1-9 22:24
外模的质量 F4系列的就从没超过FC里面的,尤其是歼10的机模
我准备自己做外模,BMS这样的游戏,应该尽量少用这些商业软件的模型
外模的质量 F4系列的就从没超过FC里面的,尤其是歼10的机模
我准备自己做外模,BMS这样的游戏,应该尽量少用这些商业软件的模型