Active flutter suppression control law definition via least squares synthesis
Author:
Affiliation:
1. Northrop Corp., Aircraft Group, Hawthorne, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1980-765
Reference6 articles.
1. Hwang, C., Winther, B.A., and Mills, G.R. "Demonstration of Active WingfStore Flutter Suppression Systems," AFFDL Technical Report TR-78-65, June 1978.
2. Recent development of the YF-17 active flutter suppression system
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Active control of aerofoil flutter;AIAA Journal;1987-08
2. Application of optimal control techniques to aircraft flutter suppression and load alleviation;23rd Structures, Structural Dynamics and Materials Conference;1982-05-10
3. Wing/Store Flutter Suppression Investigation;Journal of Aircraft;1981-11
4. Recent Development of the YF-17 Active Flutter Suppression System;Journal of Aircraft;1981-07
5. Recent development of the YF-17 active flutter suppression system;21st Structures, Structural Dynamics, and Materials Conference;1980-05-12
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