Missile Direccted by Maneuverable Actuators

Authors

  • Dr. M. Sureshkumar  Department of computer Science and Engineering, Sri Ramakrishna Engineering College, Coimbatore, Tamil Nadu, India
  • R. Vignesh   Department of computer Science and Engineering, Sri Ramakrishna Engineering College, Coimbatore, Tamil Nadu, India
  • S.Vinotha  Department of computer Science and Engineering, Sri Ramakrishna Engineering College, Coimbatore, Tamil Nadu, India
  • S. Priyadarshini  Department of computer Science and Engineering, Sri Ramakrishna Engineering College, Coimbatore, Tamil Nadu, India

Keywords:

Wifi, LPC2292, ARM7, MATLAB, ZEM, DOF,DTMF, RF,OLSM

Abstract

This paper presents the survey of several embedded Missile directed by maneuverable actuators system. Using Arduino board and architecture like Wifi module and using servo motors. This paper is been processed to reduce the man power and to automate the entire missile system. This leads to less human error and more accurate processing of the system. This surveys depicts the various methodology to automate the missile directed by maneuverable actuators system. The different ideas related to the automation system and the design modules will help to bring out various methods regarding the automation system.

References

  1. A.M. Anushree Kirthika  (2014), "Missile Detection and Automatic Destroy System"Volume 4, Number 1, pp. 1-6.
  2. Ashish Jadhav, Mahesh Kumbhar, and Meenakshi Pawar"Cell Phone Controlled Ground Combat Vehicle(July 2012), "International Journal of Computer and Communication Engineering, Vol. 1, No. 2, July 2012.
  3. Deshmukh Abhijeet B.1, K SenthilKumar2,Prof. (Dr.) H.V.Vankudre(December 2014), " Modeling and Simulation of Multi-Axle Missile  directed  by  maneuverable  actuators Model  over Different Terrain Obstacles" Volume 4, Issue 12, December 2014.
  4. Fu-Kuang Yeh, Kai-Yuan Cheng, and Li-Chen Fu." Variable Structure-Based Nonlinear Missile Guidance/Autopilot Design With Highly Maneuverable Actuators "IEEE transaction on control systems technology,vol.12,no.6,november 2004.
  5. Harvey, C., and Stein, G.(June 2014), “Missile Flight control system,” IEEE Trans. Autom. Control AC-23(3), 378–387 (June 2014).
  6. A.Hla Myo Tun, S.San Hlaing Oo, C.Myint Myint Yi," Analysis of Phase Lead Compensator Design for Laser Guided Missile System using MATLAB"
  7. B. Kada,"Outer-Loop Sliding Mode Control Approach to Longitudinal Autopilot Missile Design"IFAC World Congress Milano, September 2, 2011
  8. Masahiko Saito,Mayur Palankar(2015), ”Embedded Systems - Missile Detection/ Interception,”IEEE transactions of Missile system 2015.
  9. Reichert, R. T.(2014), “Dynamic Scheduling of Modern-Robust-Control Autopilot Designs for Missiles,” IEEE Control Systems Magazine 12(5), 35–42 (2014).
  10. Yang Xin, Bo Qingwei  and Zhou Changsheng, "Design and Analysis of Servo Actuator Control System Based on ARM,"  6th International Conference on Machinery, Materials, Environment, Biotechnology and Computer (MMEBC 2016).

International Journal of Scientific Research in Science and Technology

Downloads

Published

2017-04-30

Issue

Volume 3, Issue 3, March-April-2017

Section

Research Articles

License

Copyright (c) IJSRST

Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.

How to Cite

[1]
Dr. M. Sureshkumar, R. Vignesh , S.Vinotha, S. Priyadarshini, " Missile Direccted by Maneuverable Actuators, International Journal of Scientific Research in Science and Technology(IJSRST), Online ISSN : 2395-602X, Print ISSN : 2395-6011, Volume 3, Issue 3, pp.266-270, March-April-2017.