The MathWorks 01-Sep-2000 Solver ode45 ZeroCross on StartTime 0.0 StopTime 60 RelTol 1e-4 AbsTol 1e-6 Refine 1 InitialStep auto FixedStep auto MaxStep auto NumModelInputs 1 NumModelOutputs 2 NumVirtualSubsystems 5 NumNonvirtSubsystems 0 NumNonVirtBlocksInModel 42 NumBlockTypeCounts 10 NumBlockSignals 22 NumBlockParams 41 NumZCEvents 0 NumNonsampledZCs 0 Name Blocks Description Aircraft Dynamics Model Elevator Deflection d (deg) Vertical Gust wGust (ft/sec) Rotary Gust qGust (rad/sec) Gain3 Gain4 Gain5 Gain6 Sum1 Sum2 Transfer Fcn.1 Transfer Fcn.2 Vertical Velocity w (ft/sec) Pitch Rate q (rad/sec)   Controller Stick Input (in) alpha (rad) q (rad/sec) Alpha-sensor Low-pass Filter Gain Gain2 Gain3 Pitch Rate Lead Filter Proportional plus integral compensator Stick Prefilter Sum Sum1 Sum2 Elevator Command (deg)   Dryden Wind Gust Models Band-Limited White Noise Q-gust model W-gust model Wg Qg   f14 u Actuator Model Aircraft Dynamics Model Angle of Attack Controller Dryden Wind Gust Models Gain Gain1 Gain2 Gain5 More Info More Info1 Nz pilot calculation Pilot Pilot G force Scope Stick Input Sum Sum1 alpha (rad) Nz Pilot (g)   More Info     More Info1     Nz pilot calculation w q Constant Derivative Derivative1 Gain1 Gain2 Product Sum1 Pilot g force (g)   Name BlockType Parent OutputSignalNames Gain Gain f14/Controller <1115.00171> Gain2 Gain f14/Controller <1117.00146> Gain3 Gain f14/Controller <1119.00146> Sum Sum f14/Controller <1122.00183> Sum1 Sum f14/Controller <1125.00183> Sum2 Sum f14/Controller <1128.00146> Gain Gain f14 <1105.00146> Gain1 Gain f14 <1096.00146> Gain2 Gain f14 <1107.00146> Gain5 Gain f14 <1112.00159> Nz Pilot (g) Outport f14   Pilot SignalGenerator f14 <1103.00146> Stick Input Scope f14   Sum Sum f14 <1099.00146> Sum1 Sum f14 <1083.00256> alpha (rad) Outport f14   Actuator Model TransferFcn f14 <1089.00183> Elevator Deflection d (deg) Inport f14/Aircraft Dynamics Model <1132.00146> Gain3 Gain f14/Aircraft Dynamics Model <1134.00146> Gain4 Gain f14/Aircraft Dynamics Model <1136.00134> Gain5 Gain f14/Aircraft Dynamics Model <1138.00134> Gain6 Gain f14/Aircraft Dynamics Model <1140.00134> Pitch Rate q (rad/sec) Outport f14/Aircraft Dynamics Model   Rotary Gust qGust (rad/sec) Inport f14/Aircraft Dynamics Model <1142.00134> Sum1 Sum f14/Aircraft Dynamics Model <1146.00134> Sum2 Sum f14/Aircraft Dynamics Model <1150.00134> Transfer Fcn.1 TransferFcn f14/Aircraft Dynamics Model <1152.00134> Transfer Fcn.2 TransferFcn f14/Aircraft Dynamics Model <1154.00134> Vertical Gust wGust (ft/sec) Inport f14/Aircraft Dynamics Model <1155.00134> Vertical Velocity w (ft/sec) Outport f14/Aircraft Dynamics Model   Angle of Attack Scope f14   Alpha-sensor Low-pass Filter TransferFcn f14/Controller <1159.00122> Elevator Command (deg) Outport f14/Controller   Pitch Rate Lead Filter TransferFcn f14/Controller <1162.00134> Proportional plus integral compensator TransferFcn f14/Controller <1164.00488> Stick Input (in) Inport f14/Controller <1165.00781> Stick Prefilter TransferFcn f14/Controller <1167.00159> alpha (rad) Inport f14/Controller <1168.00159> q (rad/sec) Inport f14/Controller <1169.00159> Band-Limited White Noise SubSystem f14/Dryden Wind Gust Models <1170.00159> Q-gust model TransferFcn f14/Dryden Wind Gust Models <1172.00159> Qg Outport f14/Dryden Wind Gust Models   W-gust model TransferFcn f14/Dryden Wind Gust Models <1175.00159> Wg Outport f14/Dryden Wind Gust Models   Constant Constant f14/Nz pilot calculation <1177.00134> Derivative Derivative f14/Nz pilot calculation <1179.00134> Derivative1 Derivative f14/Nz pilot calculation <1181.00366> Gain1 Gain f14/Nz pilot calculation <1183.00195> Gain2 Gain f14/Nz pilot calculation <1185.00171> Pilot g force (g) Outport f14/Nz pilot calculation   Product Product f14/Nz pilot calculation <1189.00159> Sum1 Sum f14/Nz pilot calculation <1193.00159> q Inport f14/Nz pilot calculation <1194.00159> w Inport f14/Nz pilot calculation <1195.00159> Pilot G force Scope Scope f14   u Inport f14 <1102.00146> BlockType # of Occurrences Gain 13 TransferFcn 9 Inport 9 Sum 8 Outport 8 SubSystem 7 Scope 3 Derivative 2 SignalGenerator 1 Product 1 Constant 1 Function Name Parent Blocks Calling string pi Q-gust model Q-gust model pi/(4*b)*[1 0] [1 pi*Vto/(4*b)] sqrt W-gust model Swg/sqrt(a^3)*[sqrt(3)*a,1] Variable Name Parent Blocks Calling string Value Ka Gain3 Ka 0.677 Kf Gain Kf -1.746 Ki Proportional plus integral compensator [Ki] -3.864 Kq Gain2 Kq 0.8156 Md Gain6 Md -6.8847 Mq Transfer Fcn.1 Gain1 [1,-Mq] Mq -0.6571 Mw Gain4 Gain2 Mw Mw -0.00592 Swg W-gust model Swg/sqrt(a^3)*[sqrt(3)*a,1] 3 Ta Actuator Model [ Ta, 1] 0.05 Tal Alpha-sensor Low-pass Filter [Tal,1] 0.3959 Ts Stick Prefilter [Ts,1] 0.1 Uo Gain3 Gain5 Constant Uo 1/Uo Uo 689.4 Vto Q-gust model [1 pi*Vto/(4*b)] 690.4 W1 Pitch Rate Lead Filter [1,W1] 2.971 W2 Pitch Rate Lead Filter [1,W2] 4.144 Zd Gain5 Zd -63.9979 Zw Transfer Fcn.2 Gain [1,-Zw] Zw -0.6385 a W-gust model W-gust model Swg/sqrt(a^3)*[sqrt(3)*a,1] [1 (2/a) 1/a^2] 2.5348 b Q-gust model Q-gust model pi/(4*b)*[1 0] [1 pi*Vto/(4*b)] 64.13 g Gain2 1/g 32.2 Name ParentBlock RTWStorageClass <1083.0026> f14/Sum1 Auto <1087.002> f14/Controller Auto <1089.0018> f14/Actuator Model Auto <1096.0015> f14/Gain1 Auto <1099.0015> f14/Sum Auto <1102.0015> f14/u Auto <1103.0015> f14/Pilot Auto <1105.0015> f14/Gain Auto <1107.0015> f14/Gain2 Auto <1110.0016> f14/Nz pilot calculation Auto <1112.0016> f14/Gain5 Auto <1115.0017> f14/Controller/Gain Auto <1117.0015> f14/Controller/Gain2 Auto <1119.0015> f14/Controller/Gain3 Auto <1122.0018> f14/Controller/Sum Auto <1125.0018> f14/Controller/Sum1 Auto <1128.0015> f14/Controller/Sum2 Auto <1132.0015> f14/Aircraft Dynamics Model/Elevator Deflection d (deg) Auto <1134.0015> f14/Aircraft Dynamics Model/Gain3 Auto <1136.0013> f14/Aircraft Dynamics Model/Gain4 Auto <1138.0013> f14/Aircraft Dynamics Model/Gain5 Auto <1140.0013> f14/Aircraft Dynamics Model/Gain6 Auto <1142.0013> f14/Aircraft Dynamics Model/Rotary Gust qGust (rad//sec) Auto <1146.0013> f14/Aircraft Dynamics Model/Sum1 Auto <1150.0013> f14/Aircraft Dynamics Model/Sum2 Auto <1152.0013> f14/Aircraft Dynamics Model/Transfer Fcn.1 Auto <1154.0013> f14/Aircraft Dynamics Model/Transfer Fcn.2 Auto <1155.0013> f14/Aircraft Dynamics Model/Vertical Gust wGust (ft//sec) Auto <1159.0012> f14/Controller/Alpha-sensor Low-pass Filter Auto <1162.0013> f14/Controller/Pitch Rate Lead Filter Auto <1164.0049> f14/Controller/Proportional plus integral compensator Auto <1165.0078> f14/Controller/Stick Input (in) Auto <1167.0016> f14/Controller/Stick Prefilter Auto <1168.0016> f14/Controller/alpha (rad) Auto <1169.0016> f14/Controller/q (rad//sec) Auto <1170.0016> f14/Dryden Wind Gust Models/Band-Limited White Noise Auto <1172.0016> f14/Dryden Wind Gust Models/Q-gust model Auto <1175.0016> f14/Dryden Wind Gust Models/W-gust model Auto <1177.0013> f14/Nz pilot calculation/Constant Auto <1179.0013> f14/Nz pilot calculation/Derivative Auto <1181.0037> f14/Nz pilot calculation/Derivative1 Auto <1183.002> f14/Nz pilot calculation/Gain1 Auto <1185.0017> f14/Nz pilot calculation/Gain2 Auto <1189.0016> f14/Nz pilot calculation/Product Auto <1193.0016> f14/Nz pilot calculation/Sum1 Auto <1194.0016> f14/Nz pilot calculation/q Auto <1195.0016> f14/Nz pilot calculation/w Auto q f14/Aircraft Dynamics Model Auto qGust f14/Dryden Wind Gust Models Auto w f14/Aircraft Dynamics Model Auto wGust f14/Dryden Wind Gust Models Auto