For Libraries For Publication Open Access Downloads About Us Contact Us
Paper Titles
Vision-Based Deformation Measurement of Loaded Three-Ring Chain
p.865
Simulation Research of the Ship Course Control System
p.871
Structure Optimization Design and Airflow Numerical Simulation for Negative Pressure Isolated Cabin
p.876
Design Based on Multi-Channel Power Acquisition and Data Teletransmission System of MSP430 Simulating SPI Interface and CS5460A Communication
p.880
One Kind of Flight Control System Design for Separation Section in Cruise Missile
p.885
Study of Shock Control of Gear-Shifting in Automatic Transmission
p.890
The Situation and Developing Prospects of Embedded Systems
p.895
DSP-Based Intelligent Split-Phase Self-Adaption Reactive Power Compensation Controller
p.900
Object Tracking with Gradient Part-Based Models
p.905

One Kind of Flight Control System Design for Separation Section in Cruise Missile

Article Preview

Abstract:

Separation section is the most complex and dramatic stage in disturbing the cruise missile during the entire flight trajectory. The characteristic of low-altitude, low-speed, non-aileron flight separation of the missile propelled by rocket was analyzed in this paper. Classic engineering methods and neural network dynamic inversion methods was used to design control system, and two different control methods were compared.

You might also be interested in these eBooks
Mechatronics and Intelligent Materials II View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 490-495)

Pages:

885-889

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.490-495.885

Citation:

Cite this paper

Online since:

March 2012

Authors:

Xiao Dong Yuan, Shi Qiao Gao

Keywords:

Dynamic Inversion, Flight Control System, Missile Patrol, Neural Network (NN)

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

© 2012 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

References

[1] Lu Shiguang, Zhen Caobai, Yang Baokui. Cruise Missile Overall Design[M]. Beijing: Astronautics Press, (2005).

Google Scholar

[2] Pan Ronglin. Missile Flight Control System[M]. Beijing. Aerospace Publishing, (2007).

Google Scholar

[3] ROBERT C. NELSON. Flight Stability and Automatic Control[M]. New York: McGraw-Hill, c1989.

Google Scholar

[4] Wu Sentang. Random Flight Missile Guidance Robust Control System Analysis and Design[M]. Beijing: National Defense Industry Press, (2010).

Google Scholar

© 2025 Trans Tech Publications Ltd. All rights are reserved, including those for text and data mining, AI training, and similar technologies. For open access content, terms of the Creative Commons licensing CC-BY are applied.
Scientific.Net is a registered trademark of Trans Tech Publications Ltd.