Towards integrated multidisciplinary synthesis of actively controlled fiber composite wings
- 1 December 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 27 (12) , 979-992
- https://doi.org/10.2514/3.45972
Abstract
No abstract availableKeywords
This publication has 77 references indexed in Scilit:
- Design of control laws for flutter suppression based on the aerodynamic energy concept and comparisons with other design methodsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Design of a multivariable flutter suppression/gust load alleviation systemJournal of Guidance, Control, and Dynamics, 1988
- Interactions between an aircraft structure and active control systemsJournal of Guidance, Control, and Dynamics, 1987
- Aeroelastic tailoring - Creative uses of unusual materialsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Interdisciplinary and Multilevel Optimum DesignPublished by Springer Nature ,1987
- Frequency domain synthesis of a robust flutter suppression control lawJournal of Guidance, Control, and Dynamics, 1986
- Aeroelastic tailoring - Theory, practice, and promiseJournal of Aircraft, 1986
- On Making Things the Best-Aeronautical Uses of OptimizationJournal of Aircraft, 1982
- Aeroservoelastic EncountersJournal of Aircraft, 1979
- YF16 active-control-system/structural dynamics interaction instabilityPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975