A Novel Optimal Control Method for Impulsive-Correction Projectile Based on Particle Swarm Optimization

This paper presents a new parametric optimization approach based on a modified particle swarm optimization (PSO) to design a class of impulsive-correction projectiles with discrete, flexible-time interval, and finite-energy control. In terms of optimal control theory, the task is described as the fo...

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Main Authors: Ruisheng Sun, Qiao Hong, Gang Zhu
Format: Article
Language:English
Published: Hindawi Limited 2016-01-01
Series:Discrete Dynamics in Nature and Society
Online Access:http://dx.doi.org/10.1155/2016/5098784
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spelling doaj-21389a9d93eb4cff8e8d7d4a51a13d0d2020-11-25T00:08:05ZengHindawi LimitedDiscrete Dynamics in Nature and Society1026-02261607-887X2016-01-01201610.1155/2016/50987845098784A Novel Optimal Control Method for Impulsive-Correction Projectile Based on Particle Swarm OptimizationRuisheng Sun0Qiao Hong1Gang Zhu2Nanjing University of Science and Technology, Nanjing 210094, ChinaChina Academy of Engineering Physics, Mianyang, Sichuan 621900, ChinaChina Academy of Engineering Physics, Mianyang, Sichuan 621900, ChinaThis paper presents a new parametric optimization approach based on a modified particle swarm optimization (PSO) to design a class of impulsive-correction projectiles with discrete, flexible-time interval, and finite-energy control. In terms of optimal control theory, the task is described as the formulation of minimum working number of impulses and minimum control error, which involves reference model linearization, boundary conditions, and discontinuous objective function. These result in difficulties in finding the global optimum solution by directly utilizing any other optimization approaches, for example, Hp-adaptive pseudospectral method. Consequently, PSO mechanism is employed for optimal setting of impulsive control by considering the time intervals between two neighboring lateral impulses as design variables, which makes the briefness of the optimization process. A modification on basic PSO algorithm is developed to improve the convergence speed of this optimization through linearly decreasing the inertial weight. In addition, a suboptimal control and guidance law based on PSO technique are put forward for the real-time consideration of the online design in practice. Finally, a simulation case coupled with a nonlinear flight dynamic model is applied to validate the modified PSO control algorithm. The results of comparative study illustrate that the proposed optimal control algorithm has a good performance in obtaining the optimal control efficiently and accurately and provides a reference approach to handling such impulsive-correction problem.http://dx.doi.org/10.1155/2016/5098784
collection DOAJ
language English
format Article
sources DOAJ
author Ruisheng Sun
Qiao Hong
Gang Zhu
spellingShingle Ruisheng Sun
Qiao Hong
Gang Zhu
A Novel Optimal Control Method for Impulsive-Correction Projectile Based on Particle Swarm Optimization
Discrete Dynamics in Nature and Society
author_facet Ruisheng Sun
Qiao Hong
Gang Zhu
author_sort Ruisheng Sun
title A Novel Optimal Control Method for Impulsive-Correction Projectile Based on Particle Swarm Optimization
title_short A Novel Optimal Control Method for Impulsive-Correction Projectile Based on Particle Swarm Optimization
title_full A Novel Optimal Control Method for Impulsive-Correction Projectile Based on Particle Swarm Optimization
title_fullStr A Novel Optimal Control Method for Impulsive-Correction Projectile Based on Particle Swarm Optimization
title_full_unstemmed A Novel Optimal Control Method for Impulsive-Correction Projectile Based on Particle Swarm Optimization
title_sort novel optimal control method for impulsive-correction projectile based on particle swarm optimization
publisher Hindawi Limited
series Discrete Dynamics in Nature and Society
issn 1026-0226
1607-887X
publishDate 2016-01-01
description This paper presents a new parametric optimization approach based on a modified particle swarm optimization (PSO) to design a class of impulsive-correction projectiles with discrete, flexible-time interval, and finite-energy control. In terms of optimal control theory, the task is described as the formulation of minimum working number of impulses and minimum control error, which involves reference model linearization, boundary conditions, and discontinuous objective function. These result in difficulties in finding the global optimum solution by directly utilizing any other optimization approaches, for example, Hp-adaptive pseudospectral method. Consequently, PSO mechanism is employed for optimal setting of impulsive control by considering the time intervals between two neighboring lateral impulses as design variables, which makes the briefness of the optimization process. A modification on basic PSO algorithm is developed to improve the convergence speed of this optimization through linearly decreasing the inertial weight. In addition, a suboptimal control and guidance law based on PSO technique are put forward for the real-time consideration of the online design in practice. Finally, a simulation case coupled with a nonlinear flight dynamic model is applied to validate the modified PSO control algorithm. The results of comparative study illustrate that the proposed optimal control algorithm has a good performance in obtaining the optimal control efficiently and accurately and provides a reference approach to handling such impulsive-correction problem.
url http://dx.doi.org/10.1155/2016/5098784
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