The Application of PID Controller in Missile Longitudinal Loop System and Its Simulation

DOI

10.2991/icadme-15.2015.395How to use a DOI?

Keywords

Missile longitudinal loop; PID controller; Stable; Stimulation; Aerodynamics

Abstract

In the traditional missile longitudinal loop design, the additional pitch angle feedback, trajectory inclination angle and attack angle outputs may cause the missile control system become unstable and cannot provide the fast and accurate control. In this paper, the author build up a longitudinal loop model, and design the missile longitudinal loop control system based on the PID controller. Through the simulation test, it draws the conclusions that the PID controller can make the system become stable. At the same time, the determination of the key parameters of aerodynamics variable and velocity can make the foundation and support to the design and development of the missile control system.

Copyright

© 2015, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

Download article (PDF)

TY  - CONF
AU  - Bo Zhang
AU  - Qixing Lv
AU  - Yuqing Lei
PY  - 2015/10
DA  - 2015/10
TI  - The Application of PID Controller in Missile Longitudinal Loop System and Its Simulation
BT  - Proceedings of the 5th International Conference on Advanced Design and Manufacturing Engineering
PB  - Atlantis Press
SP  - 2113
EP  - 2118
SN  - 2352-5401
UR  - https://doi.org/10.2991/icadme-15.2015.395
DO  - 10.2991/icadme-15.2015.395
ID  - Zhang2015/10
ER  -