Quadratic synthhesis of integrated active controls for an aeroelastic forward-swept-wing aircraft
- 1 March 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 7 (2) , 190-196
- https://doi.org/10.2514/3.8566
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Rigid body-structural mode coupling on a forward swept wing aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Flutter of forward swept wings, analyses and testsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982