Multi-dimensional Taylor Network Optimal Control of the Axisymmetric Cruise Missile Flight

Yongyan Ge, Hongsen Yan, Lingchen Xia

2018

Abstract

In this paper, we present the design of the multi-dimensional Taylor network (MTN) optimal controller in the flight control of cruise missile. The MTN optimal control, which combines the classical architecture of feedback control system and the new controller structure, it is not only suitable for the analysis of the stability of the closed-loop system, but also for the control of nonlinear systems with mechanism known or unknown models. Firstly, this paper will briefly introduce the theoretical basis of the MTN optimal control. Secondly, the characteristics of the missile mathematical model and the theory of missile control will be explained, accompanied with the design of controller. Finally, the feasibility of the method is validated through numerical simulation of the PID controller, PIDNN controller and the MTN optimal controller. The results show that the MTN optimal controller has the best control effect of them.

Paper Citation

in Harvard Style

Ge Y., Yan H. and Xia L. (2018). Multi-dimensional Taylor Network Optimal Control of the Axisymmetric Cruise Missile Flight.In 3rd International Conference on Electromechanical Control Technology and Transportation - Volume 1: ICECTT, ISBN 978-989-758-312-4, pages 156-162. DOI: 10.5220/0006966801560162

in Bibtex Style

@conference{icectt18,
author={Yongyan Ge and Hongsen Yan and Lingchen Xia},
title={Multi-dimensional Taylor Network Optimal Control of the Axisymmetric Cruise Missile Flight},
booktitle={3rd International Conference on Electromechanical Control Technology and Transportation - Volume 1: ICECTT,},
year={2018},
pages={156-162},
publisher={SciTePress},
organization={INSTICC},
doi={10.5220/0006966801560162},
isbn={978-989-758-312-4},
}

in EndNote Style

TY - CONF

JO - 3rd International Conference on Electromechanical Control Technology and Transportation - Volume 1: ICECTT,
TI - Multi-dimensional Taylor Network Optimal Control of the Axisymmetric Cruise Missile Flight
SN - 978-989-758-312-4
AU - Ge Y.
AU - Yan H.
AU - Xia L.
PY - 2018
SP - 156
EP - 162
DO - 10.5220/0006966801560162