Robust Flight Control System Design by Multiple-Delay-Model / Multiple-Design-Point Approach using Enhanced LMI Characterizations-Reference-Cited by-同舟云学术

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Robust Flight Control System Design by Multiple-Delay-Model / Multiple-Design-Point Approach using Enhanced LMI Characterizations

Published:2017 Issue:0 Volume:16 Page:45-53
ISSN:1884-0477
Container-title:AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

TOTOKI Hironori¹,OCHI Yoshimasa²

Affiliation:

1. Equipment and Structural Engineering, Graduate School of Science and Engineering, National Defense Academy

2. Department of Aerospace Engineering, National Defense Academy

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/astj/16/0/16_JSASS-D-16-00001/_pdf

Reference16 articles.

1. 1) Stevens, B. L. and Lewis, F. L.: Aircraft Control and Simulation, 2nd Edition, John Wiley & Sons, New Jersey, 2003, pp.201-208.

2. 2) Rogers, W. and Collins, D.: X-29 H∞ Controller Synthesis, AIAA J. Guidance, Control, and Dynamics, 15 (1992), pp. 962-967.

3. 4) Kawaguchi, J., Ninomiya, T. and Miyazawa, Y.: Stochastic Approach to Robust Flight Control Design Using Hierarchy-Structured Dynamic Inversion, AIAA J. Guidance, Control, and Dynamics, 34 (2011), pp.1573-1576.

4. Stochastic Robust Control Design Using Density-Ratio Estimation

5. 6) Hodgkinson, J.: Aircraft Handling Qualities, AIAA Education Series, AIAA, Virginia, 1999, pp. 62-66.

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