Stability and Robustness Analysis of a LASER Guided Missile System Using PID Controller

Mugdha Sunil Polimera; V. Kalaichelvi

doi:10.4028/www.scientific.net/AMM.666.208

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 666Stability and Robustness Analysis of a LASER...

Stability and Robustness Analysis of a LASER Guided Missile System Using PID Controller

Abstract:

A LASER Guided Missile System is used in most military operations for its known accuracy. But, a typical such system has a high order of non-linear characteristics and thus, a highly unstable performance. Such systems have a guidance and control system which acts as a flying servomechanism - an electromechanical device that positions an object according to a variable signal by reducing the error between two quantities. The guidance portion of the system develops the variable input signal. The input signal represents the desired course to the target. The missile control system operates to bring the missile onto the desired course. Thus, the output of the guidance and control system is the actual missile flight path. This paper dwells into the idea of using a PID Controller as part of the ‘control system’ in the missile, introducing stability in the system by reducing the error. The controller has been simulated using Simulink environment of MATLAB. The robustness of this PID controller, for different non-ideal environments, is tested post – tuning and is analysed based on performance criteria like overshoot, settling time etc.

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Periodical:

Applied Mechanics and Materials (Volume 666)

Pages:

208-212

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.666.208

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Online since:

October 2014

Authors:

Mugdha Sunil Polimera*, V. Kalaichelvi

Keywords:

LASER Guided Missile System, PID, Robustness, Stability Analysis

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References

[1] Garg, Garg, Design And Application Of A Lead Compensator To A Guided Missile System, Proc. of Int. Conf. on Emerging Trends in Engineering and Technology, (2013).

Google Scholar

[2] Tun, Nwe, Naing, Design Analysis Of Phase Lead Compensation For Typical Laser Guided Missile Control System Using MATLAB Bode Plots, 10th Intl. Conf. on Control, Automation, Robotics and Vision, 2008 ., pp.2332-2336.

DOI: 10.1109/icarcv.2008.4795897

Google Scholar

[3] J.H. Blakelock, Automatic Control of Aircraft and Missiles, John Wiley&Sons, 2nded., (1991).

Google Scholar

[4] Math Works, Introduction to MATLAB, the Math Works, Inc (2010).

Google Scholar

[5] RafaelYanushevsky, Modern Missile Guidance, CRC Press, Taylor&Francis Group, (2008).

Google Scholar