Design for Robust Aircraft Flight Control
Author:
Affiliation:
1. University of California, Davis, Davis, California 95616
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034497
Reference26 articles.
1. Frequency Domain-Based Pseudosliding Mode Flight Control Design
2. Sliding Mode Control Applied to Reconfigurable Flight Control Design
3. SchmidtD. K., Modern Flight Dynamics, McGraw–Hill, New York, 2012, pp. 827–835.
4. Flexible vehicle control using quantitative feedback theory
5. Frequency domain, pseudo-sliding mode control system for a flexible aircraft
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