Gust Load Alleviation for a Regional Aircraft Through a Static Output Feedback-Reference-Cited by-同舟云学术

Gust Load Alleviation for a Regional Aircraft Through a Static Output Feedback

Published:2015-09 Issue:5 Volume:52 Page:1559-1574
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Fonte Federico¹,Ricci Sergio¹,Mantegazza Paolo¹

Affiliation:

1. Dipartimento di Scienze e Tecnologie Aerospaziali, Politecnico di Milano, 27010 Milan, Italy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032995

Reference43 articles.

1. Turbulent Wind and Its Effect on Flight

2. Gust-alleviation control systems for aircraft

3. LockW. P.KordesE. E.McKayJ. M.WykesJ. H. “Flight Investigation of a Structural Mode Control System for the XB-70 Aircraft,” NASA TN-D-7420, 1973.

4. Flight test evaluation of an advanced stability augmentation system for B-52 aircraft.

5. ReganC. D.JutteC. V. “Survey of Applications of Active Control Technology for Gust Alleviation and New Challenges for Lighter-Weight Aircraft,” NASA TM-2012-216008, 2012.

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