Active control of wind-tunnel model aeroelastic response using neural networks

Citation
Rc. Scott et Le. Pado, Active control of wind-tunnel model aeroelastic response using neural networks, J GUID CON, 23(6), 2000, pp. 1100-1108
Citations number
23
Categorie Soggetti
Aereospace Engineering
Journal title
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
ISSN journal
07315090 → ACNP
Volume
23
Issue
6
Year of publication
2000
Pages
1100 - 1108
Database
ISI
SICI code
0731-5090(200011/12)23:6<1100:ACOWMA>2.0.ZU;2-T
Abstract
Under a joint research and development effort conducted by NASA and The Boe ing Company (formerly McDonnell Douglas), three neural-network-based contro l systems were developed and tested. The control systems were experimentall y evaluated using a transonic wind-tunnel model in the NASA Langley Researc h Center Transonic Dynamics Tunnel, One system used a neural network to sch edule Butter suppression control laws, another employed a neural network in a predictive control scheme, and the third employed a neural network in an inverse model control scheme. All three of these control schemes successfu lly suppressed flutter to or near the limits of the testing apparatus and r epresent the first experimental applications of neural networks to Butter s uppression. The findings of this project are summarized.