Multi-Input/Multi-Output Sliding Mode Control for a Tailless Fighter Aircraft
- 1 May 2003
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 26 (3) , 463-473
- https://doi.org/10.2514/2.5084
Abstract
No abstract availableKeywords
This publication has 21 references indexed in Scilit:
- Flight Testing of Reconfigurable Control Law on the X-36 Tailless AircraftJournal of Guidance, Control, and Dynamics, 2001
- Development of a Reconfigurable Flight Control Law for Tailless AircraftJournal of Guidance, Control, and Dynamics, 2001
- Multiple model adaptive algorithms for detecting and compensating sensor and actuator/surface failures in aircraft flight control systemsInternational Journal of Robust and Nonlinear Control, 1999
- Direct adaptive reconfigurable flight control for a tailless advanced fighter aircraftInternational Journal of Robust and Nonlinear Control, 1999
- Indirect adaptive flight control system interactionsInternational Journal of Robust and Nonlinear Control, 1999
- A control engineer's guide to sliding mode controlIEEE Transactions on Control Systems Technology, 1999
- Reconfigurable tracking control with saturationJournal of Guidance, Control, and Dynamics, 1995
- Reconfigurable flight control via multiple model adaptive control methodsIEEE Transactions on Aerospace and Electronic Systems, 1991
- Variable structure control of nonlinear multivariable systems: a tutorialProceedings of the IEEE, 1988
- Control of multivariable non-linear systems by the sliding mode methodInternational Journal of Control, 1987