2015
DOI: 10.1155/2015/723298
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Modeling and Simulation of Control Actuation System with Fuzzy‐PID Logic Controlled Brushless Motor Drives for Missiles Glider Applications

Abstract: A control actuation system has been used extensively in automotive, aerospace, and defense applications. The major challenges in modeling control actuation system are rise time, maximum peak to peak overshoot, and response to nonlinear system with percentage error. This paper addresses the challenges in modeling and real time implementation of control actuation system for missiles glider applications. As an alternative fuzzy-PID controller is proposed in BLDC motor drive followed by linkage mechanism to actuat… Show more

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Cited by 12 publications
(5 citation statements)
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References 17 publications
(17 reference statements)
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“…The automatic actuation control system used in fins and gliders to maintain constant torque performance for various dynamic loads and thermal object loads [3][4]. The drive system for a BLDC generator on current control techniques using PWM signals [5][6]. Further the development of the position and speed control for various applications between the controllers, conventional PID is the most popular controller in practice has poor dynamic behavior for non-linear loads in real-time applications.…”
Section: Highlightsmentioning
confidence: 99%
“…The automatic actuation control system used in fins and gliders to maintain constant torque performance for various dynamic loads and thermal object loads [3][4]. The drive system for a BLDC generator on current control techniques using PWM signals [5][6]. Further the development of the position and speed control for various applications between the controllers, conventional PID is the most popular controller in practice has poor dynamic behavior for non-linear loads in real-time applications.…”
Section: Highlightsmentioning
confidence: 99%
“…One of the most important subsystems of the guided missiles is the control actuation system (CAS) in the sense of orienting them towards predetermined targets at a desired accuracy level (Arulmozhiyal et al, 2015). In practical applications, the CAS which is responsible of converting the command signals generated by the missile control system into reasonable physical motion by means of the control fins is subjected to the disturbing moments originated from aerodynamic effects (Muniraj and Arulmozhiyal, 2015). These effects are in general called "hinge moment effects".…”
Section: Introductionmentioning
confidence: 99%
“…Some of the studies that have been done were speed control with fuzzy logic [3], fuzzy PID [4], and Fuzzy Genetics Algorithm [5], where the controller were tested on BLDC linear motor models. The linear model is a model that is only capable presenting the motor when in its maximum performance.…”
Section: Introductionmentioning
confidence: 99%