Research on Control Augmentation System for a Flying Wing Aircraft-Reference-Cited by-同舟云学术

Research on Control Augmentation System for a Flying Wing Aircraft

Published:2014-10 Issue: Volume:1049-1050 Page:953-956
ISSN:1662-8985
Container-title:Advanced Materials Research
language:
Short-container-title:AMR

Author:

Peng Cheng¹,Wang Xin Min¹,Qiu Chuang¹

Affiliation:

1. Northwestern Polytechnical University

Abstract

Requirements of the longitudinal control augmentation system are presented through studying the 25thChina Civil Aviation Regulations and C* flight quality evaluation criterion; The C* control augmentation scheme commonly used in modern large airliners is adopted to design the control augmentation system due to the stability and handling problems for the flying wing aircraft; The particle swarm optimization algorithm is proposed due to the parameter-scheduling difficulties in the designed control augmentation system. Numerical simulation shows that the designed C* control augmentation scheme is feasible.

Publisher

Trans Tech Publications, Ltd.

Subject

General Engineering

Link

https://www.scientific.net/AMR.1049-1050.953.pdf

Reference6 articles.

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3. K.J. Bi, W.G. Zhang and M. Zhang: Computer Simulation, Vol. 30 (2013) No. 2, p.76.

4. S.T. Wu and Y.H. Fei: Flight Control System (Beihang University Press, China 2005).

5. N.U. Rahman, J.F. Whidborne and A.K. Cooke: Proceedings of International Conference on Applied Sciences & Technology (Islamabad, Pakistan, 19th -22nd January, 2009), p.177.

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