Adaptive Sliding Mode Control Design for a Hypersonic Flight Vehicle
Author:
Affiliation:
1. University of Southern California, Los Angeles, California 90089
2. California State University, Los Angeles, California 90032
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.12596
Reference6 articles.
1. Design of Robust Control Systems for a Hypersonic Aircraft
2. Robust Nonlinear Control of a Hypersonic Aircraft
3. Control of multivariable non-linear systems by the sliding mode method
4. Adaptive sliding controller synthesis for non-linear systems
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