PID Control Based Missile Sub-Channel Simulation

Chao Bo Chen; Bing Liu; Ning He; Song Gao; Quan Pan

doi:10.4028/www.scientific.net/AMR.433-440.7011

Paper Titles

Design of the Software System on Onboard Computer for Service Robots Based on Behavior Control
p.6985

Research on Cooperative Maintenance Decision System for Power Plant
p.6992

LQR Control of Single Inverted Pendulum Based on Square Root Filter
p.6999

Speed and Load Torque Estimation of Induction Motors Based on an Adaptive Extended Kalman Filter
p.7004

PID Control Based Missile Sub-Channel Simulation
p.7011

The Dempster-Shafer Theory Is Uesd in the System of SINS
p.7017

Remote Wireless Network Monitoring Application System
p.7024

The Improved Method for Solving Permutation Problem in Frequency Domain Blind Source Separation of Speech Signals
p.7029

Real-Time Target Tracking Based on SOPC
p.7035

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 433-440PID Control Based Missile Sub-Channel Simulation

PID Control Based Missile Sub-Channel Simulation

Abstract:

The accuracy and real-time of modern missile flight control system of traditional aerodynamic can not be satisfied. In this paper a new method is presented to improve the accuracy and real-time of missiles under this condition. First of all, a missile sub-channel model of the dynamic equations and steering gear is established, then based on the established model, using PID controller to control steering gear and three channels of missile pitch, yaw, roll respectively which is called missile sub-channel PID control method, and finally making use of MATLAB/Simulink to complete the simulation. Simulation results show that compared with traditional aerodynamic control system, this method can reduce the response time of aerodynamic missile and enhance the stability of the control system obviously.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 433-440)

Pages:

7011-7016

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.433-440.7011

Citation:

Cite this paper

Online since:

January 2012

Authors:

Chao Bo Chen, Bing Liu, Ning He, Song Gao, Quan Pan

Keywords:

Missile Model, Missile Sub-Channel Control, PID Control, Simulation

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Qian Xing-fang, Lin Rui-xiong, Zhao Ya-nan., Missile flight dynamics,. Beijing. Beijing Institute of Technology Press, 2000, pp.25-67.

Google Scholar

[2] Hou Hong-lu, Zhou De-yun, Wang Wei, Guo rong, Application of fuzzy-PID control in system of photo-electric tracking, Opto-Electronic Engineering, vol. 33, pp.12-16, May (2006).

Google Scholar

[3] Wang Jian-jun, Sensitivity missile control system design and simulation, " Nanjing University of Science, s master thesis, (2003).

Google Scholar

[4] Yong Seok Choi, HoChul Lee, Autopilot design for agile missile with aerodynamic fin and side thruster, SICE Annual Conference, Fukui, 2003, pp.1476-1481.

Google Scholar

[5] Rui Hirokawa, Koichi Sato, Autopilot design for a missile with re-action- jet using coefficient diagram method, AIAA Guidance, Navigation and Control conference and Exhibit, Canada, Aug. 2001, AIAA-2001-416.

DOI: 10.2514/6.2001-4162

Google Scholar

[6] Wang Zheng-lin, Wang Kai-sheng, Chen Guo-shun, MATLAB/ Simulink and control system simulation, Beijing, Electronic Industry Press, 2005, pp.187-198.

Google Scholar

[7] Sun Chuan-jie, Easy guided bombs' ballistic characteristics and digital simulation., "Nanjing University of Science, s mater thesis, (2003).

Google Scholar