Stable adaptive fault-tolerant control of overactuated aircraft using multiple models, switching and tuning
- 10 August 1998
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Multivariable adaptive algorithms for reconfigurable flight controlIEEE Transactions on Control Systems Technology, 1997
- Adaptive control using multiple modelsIEEE Transactions on Automatic Control, 1997
- Stability of dynamic inversion control laws applied to nonlinear aircraft pitch-axis modelsInternational Journal of Control, 1996
- System identification for adaptive and reconfigurable controlJournal of Guidance, Control, and Dynamics, 1995
- Dynamic inversion: an evolving methodology for flight control designInternational Journal of Control, 1994
- Improving transient response of adaptive control systems using multiple models and switchingIEEE Transactions on Automatic Control, 1994
- H-infinity design of F/A-18A automatic Carrier Landing SystemJournal of Guidance, Control, and Dynamics, 1994