Adaptive Sliding Mode Control Design for a Hypersonic Flight Vehicle
- 1 September 2004
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 27 (5), 829-838
- https://doi.org/10.2514/1.12596
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Robust Nonlinear Control of a Hypersonic AircraftJournal of Guidance, Control, and Dynamics, 2000
- Design of Robust Control Systems for a Hypersonic AircraftJournal of Guidance, Control, and Dynamics, 1998
- On Sliding Observers for Nonlinear SystemsJournal of Dynamic Systems, Measurement, and Control, 1987
- Control of multivariable non-linear systems by the sliding mode methodInternational Journal of Control, 1987
- Adaptive sliding controller synthesis for non-linear systemsInternational Journal of Control, 1986