Performance-based adaptive fuzzy control of aircrafts

Ján Vaščák, Peter Kováčik, Kaoru Hirota, Peter Sinčák

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35 引用 (Scopus)
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摘要

Aircraft behavior can be described by a set of parameters that represent their aerodynamic properties and flight conditions. They are measured in aerodynamic tunnels under some special laboratory conditions. However, they do not fully describe all possible flight situations. Their accuracy is also limited. As considerable changes of the description occur during a flight, the use of non-adaptive autopilots, especially in combat aircrafts, is strongly limited. The removal of this obstacle is possible only by means of a continuous on-line adaptation of the aircraft model and by a consecutive adaptation of the autopilot. This paper deals with the design of a performance-adaptive, the so-called self-organizing, fuzzy controller as an autopilot. The structure of such a controller as well as the modified adaptation principle with some experiments are described here.

源语言英语
文章编号56
页(从-至)761-764
页数4
期刊IEEE International Conference on Fuzzy Systems
2
DOI
出版状态已出版 - 2001
已对外发布

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Vaščák, J., Kováčik, P., Hirota, K., & Sinčák, P. (2001). Performance-based adaptive fuzzy control of aircrafts. IEEE International Conference on Fuzzy Systems, 2, 761-764. 文章 56. https://doi.org/10.1109/FUZZ.2001.1009066