Three-channel Decoupling Control for Fighter Aircraft based on Prescribed Performance Control and Super-Twisting Extended State Observer
Author:
Affiliation:
1. Tianjin University of Technology,School of Electrical Engineering and Automation,Tianjin,China
Funder
National Natural Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx8/10587298/10587321/10588179.pdf?arnumber=10588179
Reference13 articles.
1. Numerical Analysis of Aerodynamic Characteristics of F-16
2. Design and Robustness Analysis of Fighter Aircraft Flight Control Laws
3. Robust control for uncertain nonlinear systems with state-dependent control direction
4. Stability robustness of nonlinear dynamic inversion based controller
5. Maneuverable Aircraft Flight Control Using Nonlinear Dynamic Inversion;Jia
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