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 rise time, maximum peak to peak overshoot, and response to nonlinear system with percentage error. This paper addresses the challenge...
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| Format: | Article |
| Language: | English |
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Wiley
2015-01-01
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| Series: | The Scientific World Journal |
| Online Access: | http://dx.doi.org/10.1155/2015/723298 |
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| author | Murali Muniraj Ramaswamy Arulmozhiyal |
| author_facet | Murali Muniraj Ramaswamy Arulmozhiyal |
| author_sort | Murali Muniraj |
| collection | DOAJ |
| description | 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 actuate fins in missiles and gliders. The proposed system will realize better rise time and less overshoot while operating in extreme nonlinear dynamic system conditions. A mathematical model of BLDC motor is derived in state space form. The complete control actuation system is modeled in MATLAB/Simulink environment and verified by performing simulation studies. A real time prototype of the control actuation is developed with dSPACE-1104 hardware controller and a detailed analysis is carried out to confirm the viability of the proposed system. |
| format | Article |
| id | doaj-art-e172919f440f4dee91d1c98a1913dcbc |
| institution | Kabale University |
| issn | 2356-6140 1537-744X |
| language | English |
| publishDate | 2015-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | The Scientific World Journal |
| spelling | doaj-art-e172919f440f4dee91d1c98a1913dcbc2025-02-03T05:43:57ZengWileyThe Scientific World Journal2356-61401537-744X2015-01-01201510.1155/2015/723298723298Modeling and Simulation of Control Actuation System with Fuzzy-PID Logic Controlled Brushless Motor Drives for Missiles Glider ApplicationsMurali Muniraj0Ramaswamy Arulmozhiyal1Department of Electrical and Electronics Engineering, Sona College of Technology, Salem 636005, IndiaDepartment of Electrical and Electronics Engineering, Sona College of Technology, Salem 636005, IndiaA 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 actuate fins in missiles and gliders. The proposed system will realize better rise time and less overshoot while operating in extreme nonlinear dynamic system conditions. A mathematical model of BLDC motor is derived in state space form. The complete control actuation system is modeled in MATLAB/Simulink environment and verified by performing simulation studies. A real time prototype of the control actuation is developed with dSPACE-1104 hardware controller and a detailed analysis is carried out to confirm the viability of the proposed system.http://dx.doi.org/10.1155/2015/723298 |
| spellingShingle | Murali Muniraj Ramaswamy Arulmozhiyal Modeling and Simulation of Control Actuation System with Fuzzy-PID Logic Controlled Brushless Motor Drives for Missiles Glider Applications The Scientific World Journal |
| title | Modeling and Simulation of Control Actuation System with Fuzzy-PID Logic Controlled Brushless Motor Drives for Missiles Glider Applications |
| title_full | Modeling and Simulation of Control Actuation System with Fuzzy-PID Logic Controlled Brushless Motor Drives for Missiles Glider Applications |
| title_fullStr | Modeling and Simulation of Control Actuation System with Fuzzy-PID Logic Controlled Brushless Motor Drives for Missiles Glider Applications |
| title_full_unstemmed | Modeling and Simulation of Control Actuation System with Fuzzy-PID Logic Controlled Brushless Motor Drives for Missiles Glider Applications |
| title_short | Modeling and Simulation of Control Actuation System with Fuzzy-PID Logic Controlled Brushless Motor Drives for Missiles Glider Applications |
| title_sort | modeling and simulation of control actuation system with fuzzy pid logic controlled brushless motor drives for missiles glider applications |
| url | http://dx.doi.org/10.1155/2015/723298 |
| work_keys_str_mv | AT muralimuniraj modelingandsimulationofcontrolactuationsystemwithfuzzypidlogiccontrolledbrushlessmotordrivesformissilesgliderapplications AT ramaswamyarulmozhiyal modelingandsimulationofcontrolactuationsystemwithfuzzypidlogiccontrolledbrushlessmotordrivesformissilesgliderapplications |