DocumentCode
3573474
Title
Fractional PIλ control of anti-aircraft artillery servo system
Author
Gang Yang ; Chongwei Han ; Tengfei Chen ; Jing Guo
Author_Institution
Northwest Inst. of Mech. & Electr. Eng., Xianyang, China
fYear
2014
Firstpage
4617
Lastpage
4621
Abstract
Anti-aircraft artillery servo system requires high tracking accuracy and strong robustness. In this paper, an algebraic tuning rule is presented for fractional PIλ controllers to control anti-aircraft artillery. A group of suitable parameters can be chosen out by drawing the curve describing relation between gain kp, ki and integral order λ when the crossover frequency and phase margin are given. The oscillation index is introduced to help decide appropriate crossover frequency and phase margin that should be set. Simulation results are brought to demonstrate the effectiveness and robustness of this parameter tuning method.
Keywords
PI control; aircraft control; autonomous aerial vehicles; control system synthesis; missile control; mobile robots; servomechanisms; weapons; algebraic tuning rule; anti aircraft artillery servo system; crossover frequency; cruise missile; curve describing relation; fixed-wing aircraft; fractional PIλ controllers; gain; gunship; high tracking accuracy; integral order; oscillation index; parameter tuning method; phase margin; strong robustness; tactical UAV; DC motors; Indexes; Mathematical model; Oscillators; Robustness; Servomotors; Torque; anti-aircraft artillery; fractional PIλ control; servo system;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation (WCICA), 2014 11th World Congress on
Type
conf
DOI
10.1109/WCICA.2014.7053492
Filename
7053492
Link To Document