Flight Control Using Physical Dynamic Inversion
Author:
Affiliation:
1. Technical University of Munich
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1758
Reference42 articles.
1. Decoupling in a class of nonlinear systems by output feedback
2. Decoupling in a Class of Nonlinear Systems by State Variable Feedback
3. Nonlinear Control Systems
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