Design of aerospace control systems using fractional PID controller

被引：44

作者：

Aboelela, Magdy A. S. ^{[2
]}

Ahmed, Mohamed F. ^{[1
]}

Dorrah, Hassen T. ^{[2
]}

机构：

[1] Egyptian Armed Forces, Cairo, Egypt

[2] Cairo Univ, Fac Engn, Elect Power & Machines Dept, Giza, Egypt

来源：

JOURNAL OF ADVANCED RESEARCH | 2012年 / 3卷 / 03期

关键词：

Six degree of freedom missile model; Particle swarm optimization; Fractional PID control; Matlab/Simulink;

D O I：

10.1016/j.jare.2011.07.003

中图分类号：

O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];

学科分类号：

07 ; 0710 ; 09 ;

摘要：

The goal is to control the trajectory of the flight path of six degree of freedom flying body model using fractional PID. The design of fractional PID controller for the six degree of freedom flying body is described. The parameters of fractional PID controller are optimized by particle swarm optimization (PSO) method. In the optimization process, various objective functions were considered and investigated to reflect both improved dynamics of the missile system and reduced chattering in the control signal of the controller. (C) 2011 Cairo University. Production and hosting by Elsevier B.V. All rights reserved.

引用

页码：225 / 232

页数：8

共 16 条

[1] SPACE GUIDANCE EVOLUTION - A PERSONAL NARRATIVE
BATTIN, RH
[J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1982, 5 (02) : 97 - 110
[2] Blakelock J. H., 1991, AUTOMATIC CONTROL AI
[3] Cao JY, 2006, INT J CONTROL AUTOM, V4, P775
[4] DRAPER CS, 1971, NAVIGATION, V18, P26
[5] THE DEVELOPMENT OF RADAR HOMING MISSILES
FOSSIER, MW
[J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1984, 7 (06) : 641 - 651
[6] Garnell P., 1980, GUIDED WEAPON CONTRO
[7] Haeussermann Walter, 1981, AIAA J GUIDANCE CONT, V4, P225
[8] Locke Arthur S., 1955, GUIDANCE PRINCIPLES
[9] MacKenzie Donald A., 1990, INVENTING ACCURACY H
[10] Maiti D, 2008, P 4 IEEE INT C INF A

← 1 2 →