A UAV Longitudinal Control System Design Based on QFT

Chen Yong; Jin Yong Yu; Chun Ping Zhang; Hong Wei Ma

doi:10.4028/www.scientific.net/AMM.713-715.726

Paper Titles

Design of a Laser Navigation System for Substation Inspection Robot Based on Map Matching
p.711

Research on a Current Electric Bus Battery Swapping System Based on the Cartesian Coordinate Robot
p.715

A Study of Beer Fermentation Control System Based on the Technology of Computer Control
p.719

A Study on Speed Control System Based on STC89C51
p.723

A UAV Longitudinal Control System Design Based on QFT
p.726

Research of ADRC in Application to the Servo System of Self-Propelled Gun
p.730

Simulation of Fuzzy PID Control for a Large Containership Speed at Slow Steaming Condition
p.734

Fuzzy Tuning PID Control of the Rolling Mill Main Drive System
p.739

Analysis and Evaluation of Non-Singularity Workspace of Parallel Manipulator
p.743

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 713-715A UAV Longitudinal Control System Design Based on...

A UAV Longitudinal Control System Design Based on QFT

Abstract:

In this paper, the basic principle and design procedure of the quantitative feedback theory (QFT) are summarized, then control system of a UAV is designed with the QFT theory. The QFT theory can solve the robust design problem of the UAV control system due to the model parameters uncertainty perfectly. And a method of robust design for UAV is put forward from engineering application perspective. Compared with traditional control method, the simulation result shows that the control system designed by the QFT theory not only has more perfect control effect but has significant value in the engineering application.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 713-715)

Pages:

726-729

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.713-715.726

Citation:

Cite this paper

Online since:

January 2015

Authors:

Chen Yong*, Jin Yong Yu, Chun Ping Zhang, Hong Wei Ma

Keywords:

Optimal Design, QFT, Robust Control, UAV

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] Snell S A，Stout P W. Quantitative feedback theory with a scheduled gain for full envelope longitudinal control[J]. Journal of Guidance, Control and Dynamics, 1996, 19(5): 1095～1101.

DOI: 10.2514/3.21750

Google Scholar

[2] Hess R A，Gorder P J. Quantitative feedback theory applied to the design of a rotorcraft flight control system[J]. Journal of Guidance, Control, and Dynamics, 1996, 16(4): 748～753.

DOI: 10.2514/3.21076

Google Scholar

[3] Horowitz Issac C. Survey of quantitative feedback theory[J]. International Journal of Control, 1991, 53(2): 255～291.

Google Scholar

[4] Borghesani C, Chait Y，Yaniv O. Quantitative feedback theory toolbox user manual [M]. USA: The Math Works Inc, (1994).

Google Scholar

[5] Ukpai UI, Newokah ODI, Boje E. Quantitative crossfeed and feedback design of a helicopter near hover flight. AIAA Journal of Guidance , Control and Dynamic 2000; 23(6): 1045-1054.

DOI: 10.2514/2.4646

Google Scholar