| operation Block isSum() : Boolean { |
| var sums : new Sequence; |
| sums.add('aero_atc/Radar/Calculate SNR/Sum'); |
| sums.add('aero_dap3dof/H x Omega/Sum'); |
| sums.add('aero_dap3dof/H x Omega/Sum1'); |
| sums.add('aero_dap3dof/H x Omega/Sum2'); |
| sums.add('aero_dap3dof/Reaction Jet Control/Sum'); |
| sums.add('aero_dap3dof/Reaction Jet Control/Yaw Control Law/Jet On TIme Counter/Sum'); |
| sums.add('aero_dap3dof/Reaction Jet Control/Yaw Control Law/Jet On TIme Counter/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/Yaw Control Law/Subsystem/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/Yaw Control Law/Subsystem1/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/Yaw Control Law/Subsystem2/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/Yaw Control Law/Subsystem3/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/Yaw Control Law/Sum'); |
| sums.add('aero_dap3dof/Reaction Jet Control/u Control Law/Jet On TIme Counter/Sum'); |
| sums.add('aero_dap3dof/Reaction Jet Control/u Control Law/Jet On TIme Counter/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/u Control Law/Subsystem/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/u Control Law/Subsystem1/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/u Control Law/Subsystem2/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/u Control Law/Subsystem3/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/u Control Law/Sum'); |
| sums.add('aero_dap3dof/Reaction Jet Control/v Control Law/Jet On TIme Counter/Sum'); |
| sums.add('aero_dap3dof/Reaction Jet Control/v Control Law/Jet On TIme Counter/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/v Control Law/Subsystem/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/v Control Law/Subsystem1/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/v Control Law/Subsystem2/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/v Control Law/Subsystem3/Sum1'); |
| sums.add('aero_dap3dof/Reaction Jet Control/v Control Law/Sum'); |
| sums.add('aero_dap3dof/Sum'); |
| sums.add('aero_guidance/Airframe & Autopilot/Aerodynamicsamp; Equations of Motion/ Equations of Motion (Body Axes)/Sum'); |
| sums.add('aero_guidance/Airframe & Autopilot/Aerodynamicsamp; Equations of Motion/Aerodynamics/Cm_tot'); |
| sums.add('aero_guidance/Airframe & Autopilot/Aerodynamicsamp; Equations of Motion/Aerodynamics/Cx_tot'); |
| sums.add('aero_guidance/Airframe & Autopilot/Aerodynamicsamp; Equations of Motion/Aerodynamics/Cz_tot'); |
| sums.add('aero_guidance/Airframe & Autopilot/Aerodynamicsamp; Equations of Motion/Sum2'); |
| sums.add('aero_guidance/Airframe & Autopilot/Atmosphere/Sum'); |
| sums.add('aero_guidance/Airframe & Autopilot/Atmosphere/Sum1'); |
| sums.add('aero_guidance/Airframe & Autopilot/Autopilot/Sum10'); |
| sums.add('aero_guidance/Airframe & Autopilot/Autopilot/Sum11'); |
| sums.add('aero_guidance/Airframe & Autopilot/Autopilot/Sum12'); |
| sums.add('aero_guidance/Airframe & Autopilot/Autopilot/Sum8'); |
| sums.add('aero_guidance/Airframe & Autopilot/Autopilot/Sum9'); |
| sums.add('aero_guidance/Airframe & Autopilot/Fin Actuator/Sum2'); |
| sums.add('aero_guidance/Airframe & Autopilot/Fin Actuator/Sum3'); |
| sums.add('aero_guidance/Airframe & Autopilot/Sensors/Sum'); |
| sums.add('aero_guidance/Seeker//Tracker/Range andClosing Velocity Estimates/Sum'); |
| sums.add('aero_guidance/Seeker//Tracker/Target Acquisition/Sum'); |
| sums.add('aero_guidance/Seeker//Tracker/Tracker and Sightline Rate Estimator/Estimator Filter/Sum'); |
| sums.add('aero_guidance/Seeker//Tracker/Tracker and Sightline Rate Estimator/Estimator Filter/Sum1'); |
| sums.add('aero_guidance/Seeker//Tracker/Tracker and Sightline Rate Estimator/Estimator Filter/Sum5'); |
| sums.add('aero_guidance/Seeker//Tracker/Tracker and Sightline Rate Estimator/Sum1'); |
| sums.add('aero_guidance/Seeker//Tracker/Tracker and Sightline Rate Estimator/Sum2'); |
| sums.add('aero_guidance/Seeker//Tracker/Tracker and Sightline Rate Estimator/Sum3'); |
| sums.add('aero_guidance/Seeker//Tracker/Tracker and Sightline Rate Estimator/Sum4'); |
| sums.add('aero_guidance/Seeker//Tracker/Tracker and Sightline Rate Estimator/Switch to Closed Loop Tracking/Sum5'); |
| sums.add('aero_guidance/Sum'); |
| sums.add('aero_guidance/Sum2'); |
| sums.add('aero_guidance_airframe/Aerodynamicsamp; Equations of Motion/ Equations of Motion (Body Axes)/Sum'); |
| sums.add('aero_guidance_airframe/Aerodynamicsamp; Equations of Motion/Aerodynamics/Cm_tot'); |
| sums.add('aero_guidance_airframe/Aerodynamicsamp; Equations of Motion/Aerodynamics/Cx_tot'); |
| sums.add('aero_guidance_airframe/Aerodynamicsamp; Equations of Motion/Aerodynamics/Cz_tot'); |
| sums.add('aero_guidance_airframe/Aerodynamicsamp; Equations of Motion/Sum2'); |
| sums.add('aero_guidance_airframe/Atmosphere model/Sum'); |
| sums.add('aero_guidance_airframe/Atmosphere model/Sum1'); |
| sums.add('aero_libdap/Pitch Roll Control Law/Jet On TIme Counter/Sum'); |
| sums.add('aero_libdap/Pitch Roll Control Law/Jet On TIme Counter/Sum1'); |
| sums.add('aero_libdap/Pitch Roll Control Law/Subsystem/Sum1'); |
| sums.add('aero_libdap/Pitch Roll Control Law/Subsystem1/Sum1'); |
| sums.add('aero_libdap/Pitch Roll Control Law/Subsystem2/Sum1'); |
| sums.add('aero_libdap/Pitch Roll Control Law/Subsystem3/Sum1'); |
| sums.add('aero_libdap/Pitch Roll Control Law/Sum'); |
| sums.add('aero_libdap/Yaw Control Law/Jet On TIme Counter/Sum'); |
| sums.add('aero_libdap/Yaw Control Law/Jet On TIme Counter/Sum1'); |
| sums.add('aero_libdap/Yaw Control Law/Subsystem/Sum1'); |
| sums.add('aero_libdap/Yaw Control Law/Subsystem1/Sum1'); |
| sums.add('aero_libdap/Yaw Control Law/Subsystem2/Sum1'); |
| sums.add('aero_libdap/Yaw Control Law/Subsystem3/Sum1'); |
| sums.add('aero_libdap/Yaw Control Law/Sum'); |
| sums.add('aero_librcs/Reaction Jet Control/Sum'); |
| sums.add('aero_librcs/Reaction Jet Control/Yaw Control Law/Jet On TIme Counter/Sum'); |
| sums.add('aero_librcs/Reaction Jet Control/Yaw Control Law/Jet On TIme Counter/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/Yaw Control Law/Subsystem/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/Yaw Control Law/Subsystem1/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/Yaw Control Law/Subsystem2/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/Yaw Control Law/Subsystem3/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/Yaw Control Law/Sum'); |
| sums.add('aero_librcs/Reaction Jet Control/u Control Law/Jet On TIme Counter/Sum'); |
| sums.add('aero_librcs/Reaction Jet Control/u Control Law/Jet On TIme Counter/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/u Control Law/Subsystem/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/u Control Law/Subsystem1/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/u Control Law/Subsystem2/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/u Control Law/Subsystem3/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/u Control Law/Sum'); |
| sums.add('aero_librcs/Reaction Jet Control/v Control Law/Jet On TIme Counter/Sum'); |
| sums.add('aero_librcs/Reaction Jet Control/v Control Law/Jet On TIme Counter/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/v Control Law/Subsystem/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/v Control Law/Subsystem1/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/v Control Law/Subsystem2/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/v Control Law/Subsystem3/Sum1'); |
| sums.add('aero_librcs/Reaction Jet Control/v Control Law/Sum'); |
| sums.add('aerospace/3DoF Equations of Motion / Equations of Motion (Body Axes)/Sum'); |
| sums.add('aerospace/6DoF/Equations of Motion (Configurable Subsystem)/Euler Angles/Vb x w/Sum'); |
| sums.add('aerospace/6DoF/Equations of Motion (Configurable Subsystem)/Euler Angles/sum'); |
| sums.add('aerospace/6DoF/Equations of Motion (Configurable Subsystem)/Euler Angles/sum1'); |
| sums.add('aerospace/6DoF/Equations of Motion (Configurable Subsystem)/Euler Angles/w x (Iw)/Sum'); |
| sums.add('aerospace/6DoF/Euler Angles/Vb x w/Sum'); |
| sums.add('aerospace/6DoF/Euler Angles/sum'); |
| sums.add('aerospace/6DoF/Euler Angles/sum1'); |
| sums.add('aerospace/6DoF/Euler Angles/w x (Iw)/Sum'); |
| sums.add('aerospace/6DoF/Quaternions/Vb x w/Sum'); |
| sums.add('aerospace/6DoF/Quaternions/sum'); |
| sums.add('aerospace/6DoF/Quaternions/sum1'); |
| sums.add('aerospace/6DoF/Quaternions/w x (Iw)/Sum'); |
| sums.add('aerospace/Actuators/2nd Order Non-linear Actuator/Sum2'); |
| sums.add('aerospace/Actuators/2nd Order Non-linear Actuator/Sum3'); |
| sums.add('aerospace/Actuators/2nd Order linear Actuator/Sum2'); |
| sums.add('aerospace/Actuators/2nd Order linear Actuator/Sum3'); |
| sums.add('aerospace/Atmosphere/Atmosphere model/Sum'); |
| sums.add('aerospace/Atmosphere/Atmosphere model/Sum1'); |
| sums.add('aerospace/Axes Transformations/3x3 cross product/Sum'); |
| sums.add('autopilot_plane/Plane/Aircraft Model/Aircraft Dynamics Model/Sum1'); |
| sums.add('autopilot_plane/Plane/Aircraft Model/Aircraft Dynamics Model/Sum2'); |
| sums.add('autopilot_plane/Plane/Aircraft Model/Sum'); |
| sums.add('autopilot_plane/Plane/Altitude Controller/Altitude Climb Control/Sum'); |
| sums.add('autopilot_plane/Plane/Altitude Controller/Altitude Climb Control/rate calculation/Sum2'); |
| sums.add('autopilot_plane/Plane/Altitude Controller/Altitude Hold Control/Sum'); |
| sums.add('autopilot_plane/Plane/Altitude Controller/Glideslope Control/Sum1'); |
| sums.add('autopilot_plane/Plane/Altitude Controller/Glideslope Control/Trapazoidal Integrator/sum'); |
| sums.add('autopilot_plane/Plane/ILS Glideslope Calculation/Sum'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying 2DOF PID/Sum'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying 2DOF PID/Sum1'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying 2DOF PID/Sum2'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying 2DOF PID/Sum3'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying 2DOF PID/SumD'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying Lowpass/FOS/Sum'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying Lowpass/FOS/Sum1'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying Notch/Sum'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying Notch/Sum2'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying Notch/Sum4'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying Notch/Sum5'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying Observer Form/Subtract'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying Observer Form/Subtract1'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying PID/Sum'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying PID/SumD'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying State Space/Sum'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying State Space/Sum1'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying Transfer Function/Sum1'); |
| sums.add('cstblocks/Linear Parameter Varying/Discrete Varying Transfer Function/Sum2'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying 2DOF PID/Sum'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying 2DOF PID/Sum1'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying 2DOF PID/Sum2'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying 2DOF PID/Sum3'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying 2DOF PID/SumD'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying Lowpass Filter/FOS/Sum2'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying Notch Filter/Sum'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying Notch Filter/Sum1'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying Notch Filter/Sum2'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying Notch Filter/Sum3'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying Observer Form/Subtract'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying Observer Form/Subtract1'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying PID Controller/Sum'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying PID Controller/SumD'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying State Space/Sum'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying State Space/Sum1'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying Transfer Function/Sum1'); |
| sums.add('cstblocks/Linear Parameter Varying/Varying Transfer Function/Sum2'); |
| sums.add('cstblocks/State Estimation/Kalman Filter/CalculateYhat/Add1'); |
| sums.add('cstblocks/State Estimation/Kalman Filter/Observer/Add'); |
| sums.add('cstblocks/State Estimation/Kalman Filter/Observer/MeasurementUpdate/Add1'); |
| sums.add('cstblocks/State Estimation/Kalman Filter/Observer/MeasurementUpdate/Sum'); |
| sums.add('cstblocks/State Estimation/Kalman Filter/UseCurrentEstimator/Add'); |
| sums.add('cstblocks/State Estimation/Kalman Filter/UseCurrentEstimator/Enabled Subsystem/Add1'); |
| sums.add('cstextras/DiscreteFirstOrderSection/Sum'); |
| sums.add('cstextras/DiscreteFirstOrderSection/Sum1'); |
| sums.add('cstextras/DiscreteSecondOrderSection/Sum'); |
| sums.add('cstextras/DiscreteSecondOrderSection/Sum1'); |
| sums.add('cstextras/DiscreteSecondOrderSection/Sum2'); |
| sums.add('cstextras/DiscreteSecondOrderSection/Sum3'); |
| sums.add('cstextras/FirstOrderSection/Sum2'); |
| sums.add('cstextras/SecondOrderSection/Sum2'); |
| sums.add('cstextras/SecondOrderSection/Sum4'); |
| sums.add('f14c/Aircraft DynamicsModel/Sum1'); |
| sums.add('f14c/Aircraft DynamicsModel/Sum2'); |
| sums.add('f14c/CommandGenerator/Sum1'); |
| sums.add('f14c/Controller/Sum'); |
| sums.add('f14c/Controller/Sum1'); |
| sums.add('f14c/Controller/Sum2'); |
| sums.add('f14c/Nz pilotcalculation/Sum1'); |
| sums.add('f14c/Sum'); |
| sums.add('f14c/Sum1'); |
| sums.add('f14c/Sum2'); |
| sums.add('f14n/Aircraft Dynamics Model/Sum'); |
| sums.add('f14n/Aircraft Dynamics Model/Sum1'); |
| sums.add('f14n/Aircraft Dynamics Model/Sum2'); |
| sums.add('f14n/Aircraft Dynamics Model/Sum3'); |
| sums.add('f14n/Command Generator/Sum1'); |
| sums.add('f14n/Controller/Sum'); |
| sums.add('f14n/Controller/Sum1'); |
| sums.add('f14n/Controller/Sum2'); |
| sums.add('f14n/Nz pilot calculation/Sum1'); |
| sums.add('f14n/Sum'); |
| sums.add('f14n/Sum1'); |
| sums.add('f14n/Sum2'); |
| sums.add('f14o/Aircraft DynamicsModel/Sum1'); |
| sums.add('f14o/Aircraft DynamicsModel/Sum2'); |
| sums.add('f14o/CommandGenerator/Sum1'); |
| sums.add('f14o/Controller/Sum'); |
| sums.add('f14o/Controller/Sum1'); |
| sums.add('f14o/Controller/Sum2'); |
| sums.add('f14o/Nz pilotcalculation/Sum1'); |
| sums.add('f14o/Sum'); |
| sums.add('f14o/Sum1'); |
| sums.add('f14o/Sum2'); |
| sums.add('simulink/Additional Math & Discrete/Additional Discrete/Fixed-Point State-Space/Sum Output Equation'); |
| sums.add('simulink/Additional Math & Discrete/Additional Discrete/Fixed-Point State-Space/Sum State Equation'); |
| sums.add('simulink/Additional Math & Discrete/Additional Discrete/Transfer Fcn Direct Form II Time Varying/Sum'); |
| sums.add('simulink/Additional Math & Discrete/Additional Discrete/Transfer Fcn Direct Form II/Sum'); |
| sums.add('simulink/Additional Math & Discrete/Additional Math: Increment - Decrement/Decrement Real World/FixPt Sum1'); |
| sums.add('simulink/Additional Math & Discrete/Additional Math: Increment - Decrement/Decrement Stored Integer/FixPt Sum1'); |
| sums.add('simulink/Additional Math & Discrete/Additional Math: Increment - Decrement/Decrement To Zero/FixPt Sum1'); |
| sums.add('simulink/Additional Math & Discrete/Additional Math: Increment - Decrement/Decrement Time To Zero/FixPt Sum1'); |
| sums.add('simulink/Additional Math & Discrete/Additional Math: Increment - Decrement/Increment Real World/FixPt Sum1'); |
| sums.add('simulink/Additional Math & Discrete/Additional Math: Increment - Decrement/Increment Stored Integer/FixPt Sum1'); |
| sums.add('simulink/Commonly Used Blocks/Sum'); |
| sums.add('simulink/Continuous/PID Controller (2DOF)/Sum'); |
| sums.add('simulink/Continuous/PID Controller (2DOF)/Sum1'); |
| sums.add('simulink/Continuous/PID Controller (2DOF)/Sum2'); |
| sums.add('simulink/Continuous/PID Controller (2DOF)/Sum3'); |
| sums.add('simulink/Continuous/PID Controller (2DOF)/SumD'); |
| sums.add('simulink/Continuous/PID Controller/Sum'); |
| sums.add('simulink/Continuous/PID Controller/SumD'); |
| sums.add('simulink/Discontinuities/Coulombamp; Viscous Friction/Sum'); |
| sums.add('simulink/Discontinuities/Dead Zone Dynamic/Diff'); |
| sums.add('simulink/Discontinuities/Rate Limiter Dynamic/Difference Inputs1'); |
| sums.add('simulink/Discontinuities/Rate Limiter Dynamic/Difference Inputs2'); |
| sums.add('simulink/Discrete/Difference/Diff'); |
| sums.add('simulink/Discrete/Discrete Derivative/Diff'); |
| sums.add('simulink/Discrete/Discrete PID Controller (2DOF)/Sum'); |
| sums.add('simulink/Discrete/Discrete PID Controller (2DOF)/Sum1'); |
| sums.add('simulink/Discrete/Discrete PID Controller (2DOF)/Sum2'); |
| sums.add('simulink/Discrete/Discrete PID Controller (2DOF)/Sum3'); |
| sums.add('simulink/Discrete/Discrete PID Controller (2DOF)/SumD'); |
| sums.add('simulink/Discrete/Discrete PID Controller/Sum'); |
| sums.add('simulink/Discrete/Discrete PID Controller/SumD'); |
| sums.add('simulink/Discrete/First-Order Hold/Output'); |
| sums.add('simulink/Discrete/First-Order Hold/Sum'); |
| sums.add('simulink/Discrete/First-Order Hold/Sum2'); |
| sums.add('simulink/Discrete/Transfer Fcn First Order/Diff'); |
| sums.add('simulink/Discrete/Transfer Fcn First Order/Sum'); |
| sums.add('simulink/Discrete/Transfer Fcn Lead or Lag/Sum'); |
| sums.add('simulink/Discrete/Transfer Fcn Real Zero/Sum'); |
| sums.add('simulink/Lookup Tables/Cosine/Cosine/Handle Quarter Symmetry Cosine/Amp25'); |
| sums.add('simulink/Lookup Tables/Cosine/Cosine/Handle Quarter Symmetry Cosine/Amp75'); |
| sums.add('simulink/Lookup Tables/Cosine/Cosine/Handle Quarter Symmetry Cosine/p25mA'); |
| sums.add('simulink/Lookup Tables/Cosine/Cosine/Handle Quarter Symmetry Cosine/p75mA'); |
| sums.add('simulink/Lookup Tables/Sine/Sine/Handle Quarter Symmetry Sine/Amp50'); |
| sums.add('simulink/Lookup Tables/Sine/Sine/Handle Quarter Symmetry Sine/p50mA'); |
| sums.add('simulink/Math Operations/Add'); |
| sums.add('simulink/Math Operations/Subtract'); |
| sums.add('simulink/Math Operations/Sum'); |
| sums.add('simulink/Math Operations/Sum of Elements'); |
| sums.add('simulink/Model Verification/Check Discrete Gradient/Sum'); |
| sums.add('simulink/Model-Wide Utilities/Timed-Based Linearization/Sum'); |
| sums.add('simulink/Quick Insert/Discrete/Difference/Diff'); |
| sums.add('simulink/Quick Insert/Discrete/Discrete Derivative/Diff'); |
| sums.add('simulink/Quick Insert/Lookup Tables/Cosine Lookup/Cosine/Handle Quarter Symmetry Cosine/Amp25'); |
| sums.add('simulink/Quick Insert/Lookup Tables/Cosine Lookup/Cosine/Handle Quarter Symmetry Cosine/Amp75'); |
| sums.add('simulink/Quick Insert/Lookup Tables/Cosine Lookup/Cosine/Handle Quarter Symmetry Cosine/p25mA'); |
| sums.add('simulink/Quick Insert/Lookup Tables/Cosine Lookup/Cosine/Handle Quarter Symmetry Cosine/p75mA'); |
| sums.add('simulink/Quick Insert/Lookup Tables/Exponential Lookup/Cosine/Handle Quarter Symmetry Cosine/Amp25'); |
| sums.add('simulink/Quick Insert/Lookup Tables/Exponential Lookup/Cosine/Handle Quarter Symmetry Cosine/Amp75'); |
| sums.add('simulink/Quick Insert/Lookup Tables/Exponential Lookup/Cosine/Handle Quarter Symmetry Cosine/p25mA'); |
| sums.add('simulink/Quick Insert/Lookup Tables/Exponential Lookup/Cosine/Handle Quarter Symmetry Cosine/p75mA'); |
| sums.add('simulink/Quick Insert/Lookup Tables/Exponential Lookup/Sine/Handle Quarter Symmetry Sine/Amp50'); |
| sums.add('simulink/Quick Insert/Lookup Tables/Exponential Lookup/Sine/Handle Quarter Symmetry Sine/p50mA'); |
| sums.add('simulink/Quick Insert/Lookup Tables/SinCos Lookup/Cosine/Handle Quarter Symmetry Cosine/Amp25'); |
| sums.add('simulink/Quick Insert/Lookup Tables/SinCos Lookup/Cosine/Handle Quarter Symmetry Cosine/Amp75'); |
| sums.add('simulink/Quick Insert/Lookup Tables/SinCos Lookup/Cosine/Handle Quarter Symmetry Cosine/p25mA'); |
| sums.add('simulink/Quick Insert/Lookup Tables/SinCos Lookup/Cosine/Handle Quarter Symmetry Cosine/p75mA'); |
| sums.add('simulink/Quick Insert/Lookup Tables/SinCos Lookup/Sine/Handle Quarter Symmetry Sine/Amp50'); |
| sums.add('simulink/Quick Insert/Lookup Tables/SinCos Lookup/Sine/Handle Quarter Symmetry Sine/p50mA'); |
| sums.add('simulink/Quick Insert/Lookup Tables/Sine Lookup/Sine/Handle Quarter Symmetry Sine/Amp50'); |
| sums.add('simulink/Quick Insert/Lookup Tables/Sine Lookup/Sine/Handle Quarter Symmetry Sine/p50mA'); |
| sums.add('simulink/Quick Insert/Math Operations/Minus'); |
| sums.add('simulink/Sources/Chirp Signal/Sum'); |
| sums.add('simulink/Sources/Counter Free-Running/Increment Real World/FixPt Sum1'); |
| sums.add('simulink/Sources/Counter Limited/Increment Real World/FixPt Sum1'); |
| sums.add('simulink/Sources/Ramp/Output'); |
| sums.add('simulink/Sources/Ramp/Sum'); |
| sums.add('simulink/Sources/Repeating Sequence Interpolated/LimitedCounter/Increment Real World/FixPt Sum1'); |
| sums.add('simulink/Sources/Repeating Sequence Stair/LimitedCounter/Increment Real World/FixPt Sum1'); |
| sums.add('simulink/Sources/Repeating Sequence/Sum'); |
| sums.add('simulink_need_slupdate/PID Controller (with Approximate Derivative)/Sum'); |
| sums.add('simulink_need_slupdate/PID Controller (with Approximate Derivative)/Sum1'); |
| sums.add('simulink_need_slupdate/PID Controller/Sum'); |
| sums.add('slexAircraftPitchControlExample/Aircraft Dynamic Model/Pitch Channel/Sum'); |
| sums.add('slexAircraftPitchControlExample/Aircraft Dynamic Model/Sum1'); |
| sums.add('slexAircraftPitchControlExample/Aircraft Dynamic Model/Sum2'); |
| sums.add('slexAircraftPitchControlExample/Aircraft Dynamic Model/Vertical Channel/Sum'); |
| sums.add('slexAircraftPitchControlExample/Controllers/AnalogControl/Sum'); |
| sums.add('slexAircraftPitchControlExample/Controllers/AnalogControl/Sum2'); |
| sums.add('slexAircraftPitchControlExample/Controllers/DigitalControl/Sum1'); |
| sums.add('slexAircraftPitchControlExample/Controllers/DigitalControl/Sum2'); |
| sums.add('slexAircraftPitchControlExample/Controllers/DigitalControl/Sum3'); |
| sums.add('slexAircraftPitchControlExample/Dryden Wind Gust/Sum'); |
| sums.add('slexAircraftPitchControlExample/Variant Actuator/Linear Actuator Subsystem/Sum'); |
| |
| if (self.sourceBlockRef <> null) { |
| var src = self.sourceBlockRef; |
| return sums.includes(src.qualifier + "/" + src.name); |
| } |
| return false; |
| } |
| |
| operation Block isGain() : Boolean { |
| var gains : new Sequence; |
| gains.add('aero_atc/Radar/Calculate Antenna Area/m//NM'); |
| gains.add('aero_atc/Radar/Calculate Noise of Antenna/Gain'); |
| gains.add('aero_atc/Radar/Estimate Range/NM//m'); |
| gains.add('aero_atc/Radar/Watts'); |
| gains.add('aero_atc/aircraft/m//NM'); |
| gains.add('aero_atc/weather/m//NM'); |
| gains.add('aero_atc/weather/m//NM '); |
| gains.add('aero_dap3dof/Pitch Acceleration'); |
| gains.add('aero_dap3dof/Reaction Jet Control/Yaw Control Law/2*alphs//( alph + alphs )'); |
| gains.add('aero_dap3dof/Reaction Jet Control/Yaw Control Law/Subsystem/1//(2*alph)'); |
| gains.add('aero_dap3dof/Reaction Jet Control/Yaw Control Law/Subsystem1/1//(2*alph)'); |
| gains.add('aero_dap3dof/Reaction Jet Control/Yaw Control Law/Subsystem2/1//(2*alph)'); |
| gains.add('aero_dap3dof/Reaction Jet Control/Yaw Control Law/Subsystem3/1//(2*alph)'); |
| gains.add('aero_dap3dof/Reaction Jet Control/Yaw Control Law/divide by 2'); |
| gains.add('aero_dap3dof/Reaction Jet Control/u Control Law/2*alphs//( alph + alphs )'); |
| gains.add('aero_dap3dof/Reaction Jet Control/u Control Law/Subsystem/1//(2*alph)'); |
| gains.add('aero_dap3dof/Reaction Jet Control/u Control Law/Subsystem1/1//(2*alph)'); |
| gains.add('aero_dap3dof/Reaction Jet Control/u Control Law/Subsystem2/1//(2*alph)'); |
| gains.add('aero_dap3dof/Reaction Jet Control/u Control Law/Subsystem3/1//(2*alph)'); |
| gains.add('aero_dap3dof/Reaction Jet Control/u Control Law/divide by 2'); |
| gains.add('aero_dap3dof/Reaction Jet Control/v Control Law/2*alphs//( alph + alphs )'); |
| gains.add('aero_dap3dof/Reaction Jet Control/v Control Law/Subsystem/1//(2*alph)'); |
| gains.add('aero_dap3dof/Reaction Jet Control/v Control Law/Subsystem1/1//(2*alph)'); |
| gains.add('aero_dap3dof/Reaction Jet Control/v Control Law/Subsystem2/1//(2*alph)'); |
| gains.add('aero_dap3dof/Reaction Jet Control/v Control Law/Subsystem3/1//(2*alph)'); |
| gains.add('aero_dap3dof/Reaction Jet Control/v Control Law/divide by 2'); |
| gains.add('aero_guidance/Airframe & Autopilot/Aerodynamics & Equations of Motion/ Equations of Motion (Body Axes)/1//Iyy'); |
| gains.add('aero_guidance/Airframe & Autopilot/Aerodynamics & Equations of Motion/ Equations of Motion (Body Axes)/1//mass'); |
| gains.add('aero_guidance/Airframe & Autopilot/Aerodynamics & Equations of Motion/ Equations of Motion (Body Axes)/Gravity/Gain'); |
| gains.add('aero_guidance/Airframe & Autopilot/Aerodynamics & Equations of Motion/ Equations of Motion (Body Axes)/Gravity/Gain2'); |
| gains.add('aero_guidance/Airframe & Autopilot/Aerodynamics & Equations of Motion/ Equations of Motion (Body Axes)/Matrix Gain'); |
| gains.add('aero_guidance/Airframe & Autopilot/Aerodynamics & Equations of Motion/ Equations of Motion (Body Axes)/Transform to Earth Axes/Gain'); |
| gains.add('aero_guidance/Airframe & Autopilot/Aerodynamics & Equations of Motion/Aerodynamics/Body Rate'); |
| gains.add('aero_guidance/Airframe & Autopilot/Aerodynamics & Equations of Motion/Aerodynamics/Fins/Cm'); |
| gains.add('aero_guidance/Airframe & Autopilot/Aerodynamics & Equations of Motion/Aerodynamics/Fins/Cx'); |
| gains.add('aero_guidance/Airframe & Autopilot/Aerodynamics & Equations of Motion/Aerodynamics/Fins/Cz'); |
| gains.add('aero_guidance/Airframe & Autopilot/Aerodynamics & Equations of Motion/Aerodynamics/Q'); |
| gains.add('aero_guidance/Airframe & Autopilot/Aerodynamics & Equations of Motion/Aerodynamics/S_ref'); |
| gains.add('aero_guidance/Airframe & Autopilot/Aerodynamics & Equations of Motion/Aerodynamics/S_ref '); |
| gains.add('aero_guidance/Airframe & Autopilot/Aerodynamics & Equations of Motion/Aerodynamics/S_ref X d_ref'); |
| gains.add('aero_guidance/Airframe & Autopilot/Atmosphere/1//T0'); |
| gains.add('aero_guidance/Airframe & Autopilot/Atmosphere/Lapse Rate'); |
| gains.add('aero_guidance/Airframe & Autopilot/Atmosphere/P0'); |
| gains.add('aero_guidance/Airframe & Autopilot/Atmosphere/g//R'); |
| gains.add('aero_guidance/Airframe & Autopilot/Atmosphere/gamma*R'); |
| gains.add('aero_guidance/Airframe & Autopilot/Atmosphere/rho0'); |
| gains.add('aero_guidance/Airframe & Autopilot/Autopilot/Anti-Windup Gain'); |
| gains.add('aero_guidance/Airframe & Autopilot/Fin Actuator/2*zeta * wn'); |
| gains.add('aero_guidance/Airframe & Autopilot/Fin Actuator/wn^2'); |
| gains.add('aero_guidance/Airframe & Autopilot/Sensors/l'); |
| gains.add('aero_guidance/Airframe & Autopilot/l'); |
| gains.add('aero_guidance/Guidance/Proportional Navigation Gain'); |
| gains.add('aero_guidance/Seeker//Tracker/Radome Aberration'); |
| gains.add('aero_guidance/Seeker//Tracker/Range and Closing Velocity Estimates/Bandwidth of Estimator'); |
| gains.add('aero_guidance/Seeker//Tracker/Range and Closing Velocity Estimates/Rdot ---> Vc'); |
| gains.add('aero_guidance/Seeker//Tracker/Tracker and Sightline Rate Estimator/Estimator Filter/wn_hom'); |
| gains.add('aero_guidance/Seeker//Tracker/Tracker and Sightline Rate Estimator/Estimator Filter/wn_hom '); |
| gains.add('aero_guidance/Seeker//Tracker/Tracker and Sightline Rate Estimator/Gimbal'); |
| gains.add('aero_guidance/Seeker//Tracker/Tracker and Sightline Rate Estimator/Radome Aberration'); |
| gains.add('aero_guidance/Seeker//Tracker/Tracker and Sightline Rate Estimator/Receiver'); |
| gains.add('aero_guidance/Seeker//Tracker/Tracker and Sightline Rate Estimator/Tracking Gain'); |
| gains.add('aero_guidance/Target Position/Gain'); |
| gains.add('aero_guidance_airframe/Aerodynamics & Equations of Motion/ Equations of Motion (Body Axes)/1//Iyy'); |
| gains.add('aero_guidance_airframe/Aerodynamics & Equations of Motion/ Equations of Motion (Body Axes)/1//mass'); |
| gains.add('aero_guidance_airframe/Aerodynamics & Equations of Motion/ Equations of Motion (Body Axes)/Gravity/Gain'); |
| gains.add('aero_guidance_airframe/Aerodynamics & Equations of Motion/ Equations of Motion (Body Axes)/Gravity/Gain2'); |
| gains.add('aero_guidance_airframe/Aerodynamics & Equations of Motion/ Equations of Motion (Body Axes)/Matrix Gain'); |
| gains.add('aero_guidance_airframe/Aerodynamics & Equations of Motion/ Equations of Motion (Body Axes)/Transform to Earth Axes/Gain'); |
| gains.add('aero_guidance_airframe/Aerodynamics & Equations of Motion/Aerodynamics/Body Rate'); |
| gains.add('aero_guidance_airframe/Aerodynamics & Equations of Motion/Aerodynamics/Dynamic Pressure '); |
| gains.add('aero_guidance_airframe/Aerodynamics & Equations of Motion/Aerodynamics/Fins/Cm'); |
| gains.add('aero_guidance_airframe/Aerodynamics & Equations of Motion/Aerodynamics/Fins/Cx'); |
| gains.add('aero_guidance_airframe/Aerodynamics & Equations of Motion/Aerodynamics/Fins/Cz'); |
| gains.add('aero_guidance_airframe/Aerodynamics & Equations of Motion/Aerodynamics/S_ref'); |
| gains.add('aero_guidance_airframe/Aerodynamics & Equations of Motion/Aerodynamics/S_ref * d_ref'); |
| gains.add('aero_guidance_airframe/Aerodynamics & Equations of Motion/Aerodynamics/S_ref '); |
| gains.add('aero_guidance_airframe/Atmosphere model/1//T0'); |
| gains.add('aero_guidance_airframe/Atmosphere model/Lapse Rate'); |
| gains.add('aero_guidance_airframe/Atmosphere model/P0'); |
| gains.add('aero_guidance_airframe/Atmosphere model/g//R'); |
| gains.add('aero_guidance_airframe/Atmosphere model/gamma*R'); |
| gains.add('aero_guidance_airframe/Atmosphere model/rho0'); |
| gains.add('aero_libdap/Pitch Roll Control Law/2*alphs//( alph + alphs )'); |
| gains.add('aero_libdap/Pitch Roll Control Law/Subsystem/1//(2*alph)'); |
| gains.add('aero_libdap/Pitch Roll Control Law/Subsystem1/1//(2*alph)'); |
| gains.add('aero_libdap/Pitch Roll Control Law/Subsystem2/1//(2*alph)'); |
| gains.add('aero_libdap/Pitch Roll Control Law/Subsystem3/1//(2*alph)'); |
| gains.add('aero_libdap/Pitch Roll Control Law/divide by 2'); |
| gains.add('aero_libdap/Yaw Control Law/2*alphs//( alph + alphs )'); |
| gains.add('aero_libdap/Yaw Control Law/Subsystem/1//(2*alph)'); |
| gains.add('aero_libdap/Yaw Control Law/Subsystem1/1//(2*alph)'); |
| gains.add('aero_libdap/Yaw Control Law/Subsystem2/1//(2*alph)'); |
| gains.add('aero_libdap/Yaw Control Law/Subsystem3/1//(2*alph)'); |
| gains.add('aero_libdap/Yaw Control Law/divide by 2'); |
| gains.add('aero_librcs/Reaction Jet Control/Yaw Control Law/2*alphs//( alph + alphs )'); |
| gains.add('aero_librcs/Reaction Jet Control/Yaw Control Law/Subsystem/1//(2*alph)'); |
| gains.add('aero_librcs/Reaction Jet Control/Yaw Control Law/Subsystem1/1//(2*alph)'); |
| gains.add('aero_librcs/Reaction Jet Control/Yaw Control Law/Subsystem2/1//(2*alph)'); |
| gains.add('aero_librcs/Reaction Jet Control/Yaw Control Law/Subsystem3/1//(2*alph)'); |
| gains.add('aero_librcs/Reaction Jet Control/Yaw Control Law/divide by 2'); |
| gains.add('aero_librcs/Reaction Jet Control/u Control Law/2*alphs//( alph + alphs )'); |
| gains.add('aero_librcs/Reaction Jet Control/u Control Law/Subsystem/1//(2*alph)'); |
| gains.add('aero_librcs/Reaction Jet Control/u Control Law/Subsystem1/1//(2*alph)'); |
| gains.add('aero_librcs/Reaction Jet Control/u Control Law/Subsystem2/1//(2*alph)'); |
| gains.add('aero_librcs/Reaction Jet Control/u Control Law/Subsystem3/1//(2*alph)'); |
| gains.add('aero_librcs/Reaction Jet Control/u Control Law/divide by 2'); |
| gains.add('aero_librcs/Reaction Jet Control/v Control Law/2*alphs//( alph + alphs )'); |
| gains.add('aero_librcs/Reaction Jet Control/v Control Law/Subsystem/1//(2*alph)'); |
| gains.add('aero_librcs/Reaction Jet Control/v Control Law/Subsystem1/1//(2*alph)'); |
| gains.add('aero_librcs/Reaction Jet Control/v Control Law/Subsystem2/1//(2*alph)'); |
| gains.add('aero_librcs/Reaction Jet Control/v Control Law/Subsystem3/1//(2*alph)'); |
| gains.add('aero_librcs/Reaction Jet Control/v Control Law/divide by 2'); |
| gains.add('aerospace/3DoF Equations of Motion / Equations of Motion (Body Axes)/1//Iyy'); |
| gains.add('aerospace/3DoF Equations of Motion / Equations of Motion (Body Axes)/1//mass'); |
| gains.add('aerospace/3DoF Equations of Motion / Equations of Motion (Body Axes)/Gravity/Gain'); |
| gains.add('aerospace/3DoF Equations of Motion / Equations of Motion (Body Axes)/Gravity/Gain2'); |
| gains.add('aerospace/3DoF Equations of Motion / Equations of Motion (Body Axes)/Matrix Gain'); |
| gains.add('aerospace/3DoF Equations of Motion / Equations of Motion (Body Axes)/Transform to Earth Axes/Gain'); |
| gains.add('aerospace/6DoF/Equations of Motion (Configurable Subsystem)/Euler Angles/Force ---> Acceleration'); |
| gains.add('aerospace/6DoF/Euler Angles/Force ---> Acceleration'); |
| gains.add('aerospace/6DoF/Quaternions/Force ---> Acceleration'); |
| gains.add('aerospace/6DoF/Quaternions/edot/Gain'); |
| gains.add('aerospace/Actuators/2nd Order Non-linear Actuator/2*zeta * wn'); |
| gains.add('aerospace/Actuators/2nd Order Non-linear Actuator/wn^2'); |
| gains.add('aerospace/Actuators/2nd Order linear Actuator/2*zeta * wn'); |
| gains.add('aerospace/Actuators/2nd Order linear Actuator/wn^2'); |
| gains.add('aerospace/Atmosphere/Atmosphere model/1//T0'); |
| gains.add('aerospace/Atmosphere/Atmosphere model/Lapse Rate'); |
| gains.add('aerospace/Atmosphere/Atmosphere model/P0'); |
| gains.add('aerospace/Atmosphere/Atmosphere model/g//R'); |
| gains.add('aerospace/Atmosphere/Atmosphere model/gamma*R'); |
| gains.add('aerospace/Atmosphere/Atmosphere model/rho0'); |
| gains.add('autopilot_plane/Plane/Aircraft Model/Aircraft Dynamics Model/Gain3'); |
| gains.add('autopilot_plane/Plane/Aircraft Model/Aircraft Dynamics Model/Gain4'); |
| gains.add('autopilot_plane/Plane/Aircraft Model/Aircraft Dynamics Model/Gain5'); |
| gains.add('autopilot_plane/Plane/Aircraft Model/Aircraft Dynamics Model/Gain6'); |
| gains.add('autopilot_plane/Plane/Aircraft Model/Dryden Wind Gust Models/Band-Limited White Noise/Output'); |
| gains.add('autopilot_plane/Plane/Aircraft Model/Gain'); |
| gains.add('autopilot_plane/Plane/Aircraft Model/Gain1'); |
| gains.add('autopilot_plane/Plane/Aircraft Model/Gain2'); |
| gains.add('autopilot_plane/Plane/Aircraft Model/Gain3'); |
| gains.add('autopilot_plane/Plane/Altitude Controller/Altitude Climb Control/Integral Gain1'); |
| gains.add('autopilot_plane/Plane/Altitude Controller/Altitude Climb Control/rate calculation/Integral Gain1'); |
| gains.add('autopilot_plane/Plane/Altitude Controller/Glideslope Control/Gain'); |
| gains.add('autopilot_plane/Plane/Altitude Controller/Glideslope Control/Integral Gain'); |
| gains.add('autopilot_plane/Plane/Altitude Controller/Glideslope Control/Proportional Gain'); |
| gains.add('autopilot_plane/Plane/Altitude Controller/Glideslope Control/Trapazoidal Integrator/Gain'); |
| gains.add('autopilot_plane/Plane/ft // (sec knots)'); |
| gains.add('cstblocks/Linear Parameter Varying/Varying Notch Filter/Gain'); |
| gains.add('cstextras/DiscreteSecondOrderSection/Gain1'); |
| gains.add('cstextras/SecondOrderSection/Gain'); |
| gains.add('f14c/Aircraft Dynamics Model/Gain3'); |
| gains.add('f14c/Aircraft Dynamics Model/Gain4'); |
| gains.add('f14c/Aircraft Dynamics Model/Gain5'); |
| gains.add('f14c/Aircraft Dynamics Model/Gain6'); |
| gains.add('f14c/Command Generator/Gain1'); |
| gains.add('f14c/Controller/Gain'); |
| gains.add('f14c/Controller/Gain2'); |
| gains.add('f14c/Controller/Gain3'); |
| gains.add('f14c/Gain'); |
| gains.add('f14c/Gain1'); |
| gains.add('f14c/Gain2'); |
| gains.add('f14c/Gain5'); |
| gains.add('f14c/Nz pilot calculation/Gain1'); |
| gains.add('f14c/Nz pilot calculation/Gain2'); |
| gains.add('f14n/Aircraft Dynamics Model/Gain3'); |
| gains.add('f14n/Aircraft Dynamics Model/Gain4'); |
| gains.add('f14n/Aircraft Dynamics Model/Gain5'); |
| gains.add('f14n/Aircraft Dynamics Model/Gain6'); |
| gains.add('f14n/Aircraft Dynamics Model/Gain7'); |
| gains.add('f14n/Aircraft Dynamics Model/Gain8'); |
| gains.add('f14n/Command Generator/Gain1'); |
| gains.add('f14n/Controller/Gain'); |
| gains.add('f14n/Controller/Gain2'); |
| gains.add('f14n/Controller/Gain3'); |
| gains.add('f14n/Gain'); |
| gains.add('f14n/Gain1'); |
| gains.add('f14n/Gain2'); |
| gains.add('f14n/Gain5'); |
| gains.add('f14n/Nz pilot calculation/Gain1'); |
| gains.add('f14n/Nz pilot calculation/Gain2'); |
| gains.add('f14o/Aircraft Dynamics Model/Gain3'); |
| gains.add('f14o/Aircraft Dynamics Model/Gain4'); |
| gains.add('f14o/Aircraft Dynamics Model/Gain5'); |
| gains.add('f14o/Aircraft Dynamics Model/Gain6'); |
| gains.add('f14o/Command Generator/Gain1'); |
| gains.add('f14o/Controller/Gain'); |
| gains.add('f14o/Controller/Gain2'); |
| gains.add('f14o/Controller/Gain3'); |
| gains.add('f14o/Gain'); |
| gains.add('f14o/Gain1'); |
| gains.add('f14o/Gain2'); |
| gains.add('f14o/Gain5'); |
| gains.add('f14o/Nz pilot calculation/Gain1'); |
| gains.add('f14o/Nz pilot calculation/Gain2'); |
| gains.add('simulink/Additional Math & Discrete/Additional Discrete/Fixed-Point State-Space/Direct Link Matrix D'); |
| gains.add('simulink/Additional Math & Discrete/Additional Discrete/Fixed-Point State-Space/Input Matrix B'); |
| gains.add('simulink/Additional Math & Discrete/Additional Discrete/Fixed-Point State-Space/Output Matrix C'); |
| gains.add('simulink/Additional Math & Discrete/Additional Discrete/Fixed-Point State-Space/State Matrix A'); |
| gains.add('simulink/Additional Math & Discrete/Additional Discrete/Transfer Fcn Direct Form II/DenCoef'); |
| gains.add('simulink/Additional Math & Discrete/Additional Discrete/Transfer Fcn Direct Form II/NumCoef'); |
| gains.add('simulink/Commonly Used Blocks/Gain'); |
| gains.add('simulink/Continuous/PID Controller (2DOF)/Derivative Gain'); |
| gains.add('simulink/Continuous/PID Controller (2DOF)/Filter Coefficient'); |
| gains.add('simulink/Continuous/PID Controller (2DOF)/Integral Gain'); |
| gains.add('simulink/Continuous/PID Controller (2DOF)/Proportional Gain'); |
| gains.add('simulink/Continuous/PID Controller (2DOF)/Setpoint Weighting (Derivative)'); |
| gains.add('simulink/Continuous/PID Controller (2DOF)/Setpoint Weighting (Proportional)'); |
| gains.add('simulink/Continuous/PID Controller/Derivative Gain'); |
| gains.add('simulink/Continuous/PID Controller/Filter Coefficient'); |
| gains.add('simulink/Continuous/PID Controller/Integral Gain'); |
| gains.add('simulink/Continuous/PID Controller/Proportional Gain'); |
| gains.add('simulink/Discontinuities/Coulomb & Viscous Friction/Gain'); |
| gains.add('simulink/Discontinuities/Coulomb & Viscous Friction/Gain1'); |
| gains.add('simulink/Discrete/Discrete PID Controller (2DOF)/Derivative Gain'); |
| gains.add('simulink/Discrete/Discrete PID Controller (2DOF)/Filter Coefficient'); |
| gains.add('simulink/Discrete/Discrete PID Controller (2DOF)/Integral Gain'); |
| gains.add('simulink/Discrete/Discrete PID Controller (2DOF)/Proportional Gain'); |
| gains.add('simulink/Discrete/Discrete PID Controller (2DOF)/Setpoint Weighting (Derivative)'); |
| gains.add('simulink/Discrete/Discrete PID Controller (2DOF)/Setpoint Weighting (Proportional)'); |
| gains.add('simulink/Discrete/Discrete PID Controller/Derivative Gain'); |
| gains.add('simulink/Discrete/Discrete PID Controller/Filter Coefficient'); |
| gains.add('simulink/Discrete/Discrete PID Controller/Integral Gain'); |
| gains.add('simulink/Discrete/Discrete PID Controller/Proportional Gain'); |
| gains.add('simulink/Discrete/First-Order Hold/Gain'); |
| gains.add('simulink/Discrete/Transfer Fcn First Order/Gain'); |
| gains.add('simulink/Discrete/Transfer Fcn Lead or Lag/GainPole'); |
| gains.add('simulink/Discrete/Transfer Fcn Lead or Lag/GainZero'); |
| gains.add('simulink/Discrete/Transfer Fcn Real Zero/GainZero'); |
| gains.add('simulink/Math Operations/Gain'); |
| gains.add('simulink/Math Operations/Slider Gain/Slider Gain'); |
| gains.add('simulink/Model Verification/Check Discrete Gradient/expander'); |
| gains.add('simulink/Model Verification/Check Discrete Gradient/falling'); |
| gains.add('simulink/Model Verification/Check Discrete Gradient/rising'); |
| gains.add('simulink/Ports & Subsystems/Subsystem Examples/Gain'); |
| gains.add('simulink/Signal Attributes/Data Type Propagation Examples/Gain'); |
| gains.add('simulink/Sources/Band-Limited White Noise/Output'); |
| gains.add('simulink/Sources/Chirp Signal/Gain'); |
| gains.add('simulink/User-Defined Functions/S-Function Examples/Gain'); |
| gains.add('simulink_need_slupdate/PID Controller (with Approximate Derivative)/Derivative Divisor'); |
| gains.add('simulink_need_slupdate/PID Controller (with Approximate Derivative)/Derivative Gain'); |
| gains.add('simulink_need_slupdate/PID Controller (with Approximate Derivative)/Integral Gain'); |
| gains.add('simulink_need_slupdate/PID Controller (with Approximate Derivative)/Proportional Gain'); |
| gains.add('simulink_need_slupdate/PID Controller/Derivative Gain'); |
| gains.add('simulink_need_slupdate/PID Controller/Integral Gain'); |
| gains.add('simulink_need_slupdate/PID Controller/Proportional Gain'); |
| gains.add('slexAircraftPitchControlExample/Aircraft Dynamic Model/Gain3'); |
| gains.add('slexAircraftPitchControlExample/Aircraft Dynamic Model/Gain4'); |
| gains.add('slexAircraftPitchControlExample/Aircraft Dynamic Model/Gain5'); |
| gains.add('slexAircraftPitchControlExample/Aircraft Dynamic Model/Gain6'); |
| gains.add('slexAircraftPitchControlExample/Aircraft Dynamic Model/Gain7'); |
| gains.add('slexAircraftPitchControlExample/Aircraft Dynamic Model/Pitch Channel/Gain'); |
| gains.add('slexAircraftPitchControlExample/Aircraft Dynamic Model/Vertical Channel/Gain'); |
| gains.add('slexAircraftPitchControlExample/Controllers/AnalogControl/Anti-Windup Integrator/Gain1'); |
| gains.add('slexAircraftPitchControlExample/Controllers/AnalogControl/Gain'); |
| gains.add('slexAircraftPitchControlExample/Controllers/AnalogControl/Gain2'); |
| gains.add('slexAircraftPitchControlExample/Controllers/AnalogControl/Gain3'); |
| gains.add('slexAircraftPitchControlExample/Controllers/DigitalControl/Anti-Windup Integrator/Gain1'); |
| gains.add('slexAircraftPitchControlExample/Controllers/DigitalControl/Gain'); |
| gains.add('slexAircraftPitchControlExample/Controllers/DigitalControl/Gain2'); |
| gains.add('slexAircraftPitchControlExample/Controllers/DigitalControl/Gain3'); |
| gains.add('slexAircraftPitchControlExample/Controllers/DigitalControl/Gain4'); |
| gains.add('slexAircraftPitchControlExample/Dryden Wind Gust/Gain'); |
| gains.add('slexAircraftPitchControlExample/Dryden Wind Gust/Gain1'); |
| gains.add('slexAircraftPitchControlExample/Dryden Wind Gust/Gain2'); |
| gains.add('slexAircraftPitchControlExample/Dryden Wind Gust/Gain3'); |
| gains.add('slexAircraftPitchControlExample/Dryden Wind Gust/White Noise/Output'); |
| gains.add('slexAircraftPitchControlExample/Variant Actuator/Linear Actuator Subsystem/Gain'); |
| |
| if (self.sourceBlockRef <> null) { |
| var src = self.sourceBlockRef; |
| return gains.includes(src.qualifier + "/" + src.name); |
| } |
| return false; |
| } |
