Control of an all-movable foreplane for a three surfaces aircraft wind tunnel model

Author:

Ricci S.,Scotti A.,Zanotti D.

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,Aerospace Engineering,Civil and Structural Engineering,Signal Processing,Control and Systems Engineering

Reference18 articles.

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2. S.V. Thornton, Reduction of structural loads using maneuver load control on the advanced Fighter technology integration (AFTI) mission adaptive wing, Technical Report TM-4526, NASA, 1993.

3. The active aeroelastic wing flight research program: technical program and model analytical development;Pendleton;J. Aircraft,2000

4. Adaptive wing and ow control technology;Stanewsky;Progress in Aerospace Sciences,2001

5. G.D. Miller, An active flexible wing multi-disciplinary design optimization method, Fifth AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Panama City, FL, September 7–9, 1994, AIAA-94-4412.

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