Smooth tracking control for conversion mode of a tilt-rotor aircraft with switching modeling

被引：3

作者：

Luo, Kebi ^{[1
]}

Shi, Shuang ^{[1
]}

Peng, Cong ^{[1
]}

机构：

[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 211106, Peoples R China

来源：

FRONTIERS OF INFORMATION TECHNOLOGY & ELECTRONIC ENGINEERING | 2023年 / 24卷 / 11期

基金：

中国国家自然科学基金; 中国博士后科学基金;

关键词：

Tilt-rotor aircraft; State-tracking control; Switched linear systems; Time-scheduled multiple Lyapunov function approach; Smooth interpolation; CONTROL DESIGN; FLIGHT CONTROL; SYSTEMS; STABILITY; STABILIZATION;

D O I：

10.1631/FITEE.2300266

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

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-infinity 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.

引用

页码：1591 / 1600

页数：10

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