Incremental Sliding-Mode Fault-Tolerant Flight Control
Author:
Affiliation:
1. Delft University of Technology, 2629 HS Delft, The Netherlands
2. Hong Kong Polytechnic University, Hung Hom, Kowloon, Hong Kong, People’s Republic of China
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
https://arc.aiaa.org/doi/pdf/10.2514/1.G003497
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5. Tailless aircraft flight control using multiple time scale reconfigurable sliding modes
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