For high maneuvering fighters, we propose an intelligent control method which has strong robustness in the sense that the system nonlinearities are almost completely unknown and dead-zone nonlinearity is present. Moreover, the proposed intelligent controller has very simple structure since approximators are not used and differentiation of virtual control is avoided. It is proved that all the signals in the closed-loop control system are bounded, and the attitude angle tracking error can converge to an arbitrarily small neighborhood around zero by choosing the appropriate design parameters.

Date Published: 27 November 2019
PDF: 7 pages
Proc. SPIE 11321, 2019 International Conference on Image and Video Processing, and Artificial Intelligence, 113212B (27 November 2019); doi: 10.1117/12.2547900

Published in SPIE Proceedings Vol. 11321:
2019 International Conference on Image and Video Processing, and Artificial Intelligence
Ruidan Su, Editor(s)