Continuous gust response and sensitivity derivatives using state-space models
- 1 September 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 31 (5) , 1212-1214
- https://doi.org/10.2514/3.46632
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Multidisciplinary optimization of aeroservoelastic systems using reduced-size modelsJournal of Aircraft, 1992
- Application of aeroservoelastic modeling using minimum-state unsteady aerodynamic approximationsJournal of Guidance, Control, and Dynamics, 1991
- Towards integrated multidisciplinary synthesis of actively controlled fiber composite wingsJournal of Aircraft, 1990
- Sensitivity derivatives of flutter characteristics and stability margins for aeroservoelastic designJournal of Aircraft, 1990
- Time-domain aeroservoelastic modeling using weighted unsteady aerodynamic forcesJournal of Guidance, Control, and Dynamics, 1990
- Design for Active Flutter Suppression and Gust Alleviation Using State-Space Aeroelastic ModelingJournal of Aircraft, 1982