CLC number: TP18; V279
On-line Access: 2024-08-27
Received: 2023-10-17
Revision Accepted: 2024-05-08
Crosschecked: 2023-07-06
Cited: 0
Clicked: 1680
Citations: Bibtex RefMan EndNote GB/T7714
Kebi LUO, Shuang SHI, Cong PENG. Smooth tracking control for conversionmode of a tilt-rotor aircraft with switching modeling[J]. Frontiers of Information Technology & Electronic Engineering, 2023, 24(11): 1591-1600.
@article{title="Smooth tracking control for conversionmode of a tilt-rotor aircraft with switching modeling",
author="Kebi LUO, Shuang SHI, Cong PENG",
journal="Frontiers of Information Technology & Electronic Engineering",
volume="24",
number="11",
pages="1591-1600",
year="2023",
publisher="Zhejiang University Press & Springer",
doi="10.1631/FITEE.2300266"
}
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%A Cong PENG
%J Frontiers of Information Technology & Electronic Engineering
%V 24
%N 11
%P 1591-1600
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%I Zhejiang University Press & Springer
%DOI 10.1631/FITEE.2300266
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T1 - Smooth tracking control for conversionmode of a tilt-rotor aircraft with switching modeling
A1 - Kebi LUO
A1 - Shuang SHI
A1 - Cong PENG
J0 - Frontiers of Information Technology & Electronic Engineering
VL - 24
IS - 11
SP - 1591
EP - 1600
%@ 2095-9184
Y1 - 2023
PB - Zhejiang University Press & Springer
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DOI - 10.1631/FITEE.2300266
Abstract: This paper investigates the state-tracking control problem in conversion mode of a tilt-rotor aircraft with a switching modeling method and a smooth interpolation technique. Based on the nonlinear model of the conversion mode, a switched linear model is developed by using the Jacobian linearization method and designing the switching signal based on the mast angle. Furthermore, an H∞ state-tracking control scheme is designed to deal with the conversion mode control issue. Moreover, instead of limiting the amplitude of control inputs, a smooth interpolation method is developed to create bumpless performance. Finally, the XV-15 tilt-rotor aircraft is chosen as a prototype to illustrate the effectiveness of this developed control method.
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