Control Law Synthesis for Active Flutter Suppression Using Optimal Control Theory-Reference-Cited by-同舟云学术

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Control Law Synthesis for Active Flutter Suppression Using Optimal Control Theory

Published:1979-09 Issue:5 Volume:2 Page:388-394
ISSN:0162-3192
Container-title:Journal of Guidance and Control
language:en
Short-container-title:Journal of Guidance and Control

Author:

Newsom Jerry R.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

General Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.55894

Reference14 articles.

1. Active Flutter Suppression - An Emerging Technology

2. Vepa, R. "Finite-State Modeling of Aeroelastic Systems," Ph.D. Dissertation,Department of Applied Mechanics, Stanford University, June 1975.

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