The MathWorks 01-Sep-2000 Variable Name Parent Blocks Calling string Value Mq Gain1 Mq -0.6571 Mw Gain2 Mw -0.00592 Ta Actuator Model [ Ta, 1] 0.05 Uo Gain5 1/Uo 689.4 Zw Gain Zw -0.6385 Solver ode45 ZeroCross on StartTime 0.0 StopTime 60 RelTol 1e-4 AbsTol 1e-6 Refine 1 InitialStep auto FixedStep auto MaxStep auto Name Gain Multiplication SaturateOnIntegerOverflow Gain Zw Element-wise(K.*u) on Gain1 Mq Element-wise(K.*u) on Gain2 Mw Element-wise(K.*u) on Gain5 1/Uo Element-wise(K.*u) on Name WaveForm Amplitude Frequency Units VectorParams1D Pilot square 1 0.500000 rad/sec on Name IconShape Inputs SaturateOnIntegerOverflow Sum round |++ on Sum1 round |++ on Name Numerator Denominator Actuator Model [1] [ Ta, 1] Name Description ParentSystem CompiledPortDataType <1084.0018>   f14   <1085.0018>   f14   <1088.0017>   f14   <1091.0015>   f14   <1092.0013>   f14   <1093.0013>   f14   <1094.0013>   f14   <1095.0012>   f14   <1096.0012>   f14   <1097.0012>   f14   <1098.0012>   f14   q   f14   qGust   f14   w   f14   wGust   f14   f14 Aircraft Dynamics Model Controller Dryden Wind Gust Models Band-Limited White Noise More Info More Info1 Nz pilot calculation Name f14 Parent <root> Description   Tag   Blocks 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) LinkStatus N/A BlockType # of Occurrences Block Names SubSystem 6 Aircraft Dynamics Model Controller Dryden Wind Gust Models More Info More Info1 Nz pilot calculation Gain 4 Gain Gain1 Gain2 Gain5 Scope 3 Angle of Attack Pilot G force Scope Stick Input Sum 2 Sum Sum1 Outport 2 Nz Pilot (g) alpha (rad) TransferFcn 1 Actuator Model SignalGenerator 1 Pilot Inport 1 u