Development of an Active Fault-Tolerant Flight Control Strategy
- 1 January 2008
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 31 (1), 135-147
- https://doi.org/10.2514/1.30551
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Passive fault tolerant control of a double inverted pendulum—a case studyControl Engineering Practice, 2005
- Reconfigurable control structure to prevent the rollover of heavy vehiclesControl Engineering Practice, 2005
- Historical Overview of Research in Reconfigurable Flight ControlProceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2005
- From control to supervisionAnnual Reviews in Control, 2001
- Linear parameter varying modeling of the Boeing 747-100/200 longitudinal motionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2001
- A new controller architecture for high performance, robust, and fault-tolerant controlIEEE Transactions on Automatic Control, 2001
- Linear quadratic bumpless transferAutomatica, 2000
- Multiobjective output-feedback control via LMI optimizationIEEE Transactions on Automatic Control, 1997
- H/sub ∞/ design with pole placement constraints: an LMI approachIEEE Transactions on Automatic Control, 1996
- Application of precomputed control laws in a reconfigurable aircraftflight control systemJournal of Guidance, Control, and Dynamics, 1989