Design and multifunction tests of a frequency domain-based active flutter suppression system
- 1 January 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 32 (1), 52-60
- https://doi.org/10.2514/3.46683
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Flutter suppression for the Active Flexible Wing - Control system design and experimental validationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- A summary of the Active Flexible Wing programPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- The multiple-function multi-input/multi-output digital controller system for the AFW wind tunnel modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- On-line analysis capabilities developed to support the AFW wind-tunnel testsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Maneuver load control using optimized feedforward commandsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Simulation and model reduction for the AFW programPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Active flutter suppression - Control system design and experimental validationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Hot-bench simulation of the active flexible wing wind-tunnel modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Multivariable feedback design: Concepts for a classical/modern synthesisIEEE Transactions on Automatic Control, 1981
- A Rapidly Convergent Descent Method for MinimizationThe Computer Journal, 1963