This directory contains Matlab/Simulink file of the Case Study:

- Discrete_Closed_Loop_Model.slx: Simulink Model for Matlab R2013a
- Discrete_Closed_Loop_Model_74.mdl: Simulink Model (for Older Matlab/Simulink version R2009b)
- simu_results_csv.m: produces 3 result files corresponding to 3 different simulations
       * Scénario 1, results_1.csv: 
             Vertical speed control: 0 m/s -> 2.5 m/s and Airspeed: 230 m/s constant  
             simulation duration 50 s
       * Scénario 2, results_2.csv: 
             Airspeed control: 230 m/s -> 235 m/s and Vertical speed remains zero
             simulation duration 50 s
       * Scénario 3, results_3.csv:
             Altitude change: 10000 m -> 11000 m and Airspeed: 230 m/s constant
             simulation duration 600 s
       * Scénario 4, No csv file:
             Multiple flight level changes: 10000 m -> 10500 m -> 11000 m -> 11500 m -> 8000 m and Airspeed: 230 m/s constant
             simulation duration 3000 s