@inproceedings{d3a905e7c5db4aceafc6fa596fbda55d,
title = "Fuzzy Adaptive Control for Generic Hypersonic Vehicles with Non-Affine Aerodynamic Characteristics and Output Con-straints",
abstract = "In this paper, a fuzzy adaptive control scheme is developed for a class of generic Hypersonic Vehicles (GHVs) subjected to non-affine aerodynamics. With the aid of the nonlinear mapping, the dynamics of the attitude tracking errors are transformed to a stochastic uncertain control system. By utilizing several specific smooth function vectors and estimating the boundaries of the uncertainties, the unknown changing uncertainties can be handled. Based on the mean-value theorem, the difficulties caused by non-affine aerodynamics can be circumvented. Meanwhile, two fuzzy logic systems (FLSs) are introduced for dealing with the aerodynamic nonlinearities. The constraints of the attitude angular tracking errors can be ensured simultaneously. Finally, simulation results demonstrated the effectiveness of the proposed algorithm.",
keywords = "Adaptive control, Attitude control, Flight control, Fuzzy logic system, output constraints",
author = "Xiaofeng Zhang and Kang Chen and Wenxing Fu",
note = "Publisher Copyright: {\textcopyright} 2019 Institute of Control, Robotics and Systems - ICROS.; 19th International Conference on Control, Automation and Systems, ICCAS 2019 ; Conference date: 15-10-2019 Through 18-10-2019",
year = "2019",
month = oct,
doi = "10.23919/ICCAS47443.2019.8971717",
language = "英语",
series = "International Conference on Control, Automation and Systems",
publisher = "IEEE Computer Society",
pages = "71--75",
booktitle = "ICCAS 2019 - 2019 19th International Conference on Control, Automation and Systems, Proceedings",
}