Using a custom criteria script, verify that wing oscillations are damped in multiple altitude and airspeed conditions.
Set and get custom criteria using the programmatic interface.
Use MATLAB® Unit Test to test a model, and use the TAPPlugin to create TAP results. You can use TAP with CI systems. The model is a controller-plant system of a flight controller, aircraft
Create and run a basic MATLAB® Unit Test for a test file created in Simulink® Test™. You create a test suite, run the test, and display the diagnostic report.