Model-following system with assignable error dynamics and its application to aircraft
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
General Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.19721
Reference19 articles.
1. The characteristics of model-following systems as synthesized by optimal control
2. The application of specific optimal control to the design of desensitized model following control systems
3. 4Anderson, B.D.O. and Moore, J.B., Linear Optimal Control, Prentice-Hall, Englewood Cliffs, N.J., 1971, pp.247-271.
4. Application of optimal control to perfect model following
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