Structural dynamic stability augmentation and gust alleviation of flexible aircraft-Reference-Cited by-同舟云学术

Structural dynamic stability augmentation and gust alleviation of flexible aircraft

Published:1968-08-16 Issue: Volume: Page:
ISSN:
Container-title:5th Annual Meeting and Technical Display
language:
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Author:

WYKES J.¹

Affiliation:

1. NORTH AMERICAN ROCKWELL CORP., AEROSPACE AND SYSTEMS GROUP, RESEARCH AND ENGINEERING DIV., LOS ANGELES, CALIF.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1968-1067

Reference13 articles.

1. AIAA Paper No. 66-970, December 1966 4. S h i t h , R. E . , and Lm, E. I. Linear Optimal

2. t r o l on the XI-70, AFFDL-TI-66-88, Febniary lY67 5 . Smith. R. E . Lum. E. L . and Yamamoto. T. G .

3. Application of Linear Optimal Theory t o the Control of F l e x i b l e Aircraft Ride Q u a l i t i e s , AFFDL-TR-67- 136, October 1967 6 . IYykes, J . t l , and Knight, R. J . , Progress

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