Modeling and Simulation of Control Actuation System with Fuzzy-PID Logic Controlled Brushless Motor Drives for Missiles Glider Applications
A control actuation system has been used extensively in automotive, aerospace, and defense applications.The major challenges in modeling control actuation system are Ski de fond - Homme - Skis - Skate rise time, maximum peak to peak overshoot, and response to nonlinear system with percentage error.This paper addresses the challenges in modeling and