Full Text:   <964>

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CLC number: TP18; V279

On-line Access: 2023-12-04

Received: 2023-04-13

Revision Accepted: 2023-12-05

Crosschecked: 2023-07-06

Cited: 0

Clicked: 932

Citations:  Bibtex RefMan EndNote GB/T7714

 ORCID:

Kebi LUO

https://orcid.org/0009-0001-3719-4086

Shuang SHI

https://orcid.org/0000-0001-6000-0350

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Frontiers of Information Technology & Electronic Engineering  2023 Vol.24 No.11 P.1591-1600

http://doi.org/10.1631/FITEE.2300266


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


Author(s):  Kebi LUO, Shuang SHI, Cong PENG

Affiliation(s):  College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China

Corresponding email(s):   shishuang@nuaa.edu.cn

Key Words:  Tilt-rotor aircraft, State-tracking control, Switched linear systems, Time-scheduled multiple Lyapunov function approach, Smooth interpolation


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.

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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.

基于切换系统建模的倾转旋翼机过渡模式光滑跟踪控制

罗苛比,史爽,彭聪
南京航空航天大学自动化学院,中国南京市,211106
摘要:本文使用切换建模和光滑插值技术,研究倾转旋翼机过渡模式的状态跟踪控制问题。基于过渡模式的非线性动力学模型,采用Jacobi线性化方法,并根据倾转角设计切换信号,建立线性切换系统模型。在此基础上,设计状态跟踪控制方案解决过渡模式的控制问题。该方法不直接限制控制输入的幅值,而采用改进的光滑插值方法实现无扰切换。最后,以XV-15倾转旋翼机为例,验证该控制方案的有效性。

关键词:倾转旋翼机;状态跟踪控制;线性切换系统;类时间依赖的多Lyapunov函数方法;光滑插值

Darkslateblue:Affiliate; Royal Blue:Author; Turquoise:Article

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