Initial Acceleration Suppression via Gust Alleviation Controller Using Prior Gust Information-Reference-Cited by-同舟云学术

Initial Acceleration Suppression via Gust Alleviation Controller Using Prior Gust Information

Published:2008 Issue:655 Volume:56 Page:355-362
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:ja
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

SATO Masayuki,YOKOYAMA Nobuhiro

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/56/655/56_655_355/_pdf

Reference17 articles.

1. 1) Statistical Summary of Commercial Jet Airplane Accidents: Worldwide Operations 1959-2005, Boeing, http://www. boeing.com/news/techissues/pdf/statsum.pdf

2. 2) 国交省交通政策審議会航空分科会第2回航空保安システム整備部会参考資料2-2,http://www.mlit.go.jp/singikai/koutusin/koku/hoan/2/images/sankou2_2.pdf

3. 3) Phillips, W. H.: Gust Alleviation, Performance and Dynamics of Aerospace Vehicles, NASA SP-258, 1971, pp. 505-553.

4. 4) Phillips, W. H.: Study of a Control System to Alleviate Aircraft Response to Horizontal and Vertical Gusts, NASA TN D-7278, 1973.

5. 5) Komoda, M.: Optimality Study of a Gust Alleviation System for Light Wing-Loading STOL Aircraft, NASA TN D-8180, 1976.

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