The flight data of the fuzzy logic controller developed for the altitude control of the unmanned aerial vehicle are shared in the table below. Altitude, vertical velocity inputs and controller output will be represented by 5 membership functions (zero (Z), positive small (PS), positive medium (PM), positive large (PL), positive bigger (PB)). In accordance with the data shared in the table, plot the input and output membership functions of the controller, which works according to the Mamdani inference method, as equally spaced, NB and PB trapezoidal membership functions and the others as triangle membership functions. Create the rule base suitable for the quadratic system response first column altitude information second column vertical speed third column controller output
The flight data of the fuzzy logic controller developed for the altitude control of the unmanned aerial vehicle are shared in the table below. Altitude, vertical velocity inputs and controller output will be represented by 5 membership functions (zero (Z), positive small (PS), positive medium (PM), positive large (PL), positive bigger (PB)). In accordance with the data shared in the table, plot the input and output membership functions of the controller, which works according to the Mamdani inference method, as equally spaced, NB and PB trapezoidal membership functions and the others as triangle membership functions. Create the rule base suitable for the quadratic system response
first column altitude information
second column vertical speed
third column controller output
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