Simulink Control Design™ - MathWorks

NoteTo find the location in the Simulink model corresponding to a signal in the Linearization inputs/outputs table, select the s ...

(^7) Specify multiple bound segments for assertion in the Bounds tab of the Block Parameters dialog box. In this example, enter ...

8 Simulate the model by clicking in the plot window. Alternatively, you can simulate the model from the Simulink Editor. The sof ...

You can also view the bound violations on the plot window. (^9) Modify a bound graphically. For example, to modify the upper mag ...

b Click Update block to update the new values in the Bounds tab of the Block Parameters dialog box. (^10) Disable the lower boun ...

(^11) Resimulate the model to check if bounds are satisfied. The software satisfies the specified upper magnitude bound, and the ...

Verify Model Using Simulink Control Design and Simulink Verification Blocks This example shows how to use a combination of Simul ...

8-hour velocity profile. The model is a simplified version of a velocity control loop, which adjusts the fuel flow rate to contr ...

The model has already been configured with: Linearization input and output for computing gain and phase margins Settings to com ...

In this example, the linearization input and output include the summation block with negative feedback. Change the Feedback sign ...

These parameters configure the block to: Check if the aircraft velocity exceeds the cruise velocity by 0.9 times Add an output ...

This connection causes the Assert that: PM >= 60 or if PM < 60 then v <= 0.9*vCruise block to assert and stop the simul ...

The Assert that: PM >= 60 or if PM < 60 then v <= 0.9*vCruise does not encounter the assertion condition. Therefore, t ...

When a block asserts, warnings appear in this window. You can view the details of the assertions by clicking the link in this wi ...

Verifying Frequency-Domain Characteristics of an Aircraft This example shows how to use the blocks in Linear Analysis Plots and ...

velocity profile. The Simulink model is a much simplified version of a velocity control loop which adjusts the fuel flow rate to ...

Verifying Frequency-Domain Characteristics of an Aircraft ...

The block computes the loop gain and phase margins and checks that: The gain margin is greater than 30 dB The phase margin is g ...

Verifying Frequency-Domain Characteristics of an Aircraft ...

The block shows the computed gain and phase margins in a tabular format. Clicking Show Plot button opens the tabular display. Th ...