Redesign of the feedback structure following a battle damage and/or a failure on a control surface by eigenstructure assignment
- 12 August 1991
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- A new technique for aircraft flight control reconfigurationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Totally robust control - A new concept for design of flight control systemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Active flutter suppression using eigenspace and linear quadratic design techniquesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- On the flexibility offered by state feedback in multivariable systems beyond closed loop eigenvalue assignmentIEEE Transactions on Automatic Control, 1976