Academic Journal

Incremental Backstepping Sliding-Mode Trajectory Control for Tailless Aircraft with Stability Enhancer

التفاصيل البيبلوغرافية
العنوان: Incremental Backstepping Sliding-Mode Trajectory Control for Tailless Aircraft with Stability Enhancer
المؤلفون: Zihou He, Jianbo Hu, Yingyang Wang, Jiping Cong, Linxiao Han, Maoyu Su
المصدر: Aerospace, Vol 9, Iss 7, p 352 (2022)
بيانات النشر: MDPI AG, 2022.
سنة النشر: 2022
المجموعة: LCC:Motor vehicles. Aeronautics. Astronautics
مصطلحات موضوعية: incremental control, trajectory control, tailless aircraft, sliding-mode, backstepping, Motor vehicles. Aeronautics. Astronautics, TL1-4050
الوصف: This paper presents an incremental backstepping sliding-mode (IBS) controller for trajectory control of a tailless aircraft with unknown disturbances and model uncertainties. The proposed controller is based on a nonlinear dynamic model of the tailless aircraft. A stability enhancer (SE) that limits both the rate and amplitude of the virtual control input is proposed. The stability enhancer consists of two layers. When the virtual control input approaches the edge, the first layer SE would be activated to modify the trajectory tracking error; when the virtual control input exceeds the edge, the second layer SE would reduce the control gains to make sure the virtual control input drops within the edge as soon as possible. With the help of SE, the incremental control method could be extended to outer-loop control without considering the dynamics of the inner-loop system. In addition, an adaptive estimator for state derivatives is proposed, together with IBS, allowing the controller to show excellent robustness. Finally, two simulations are presented. The first simulation shows that the system is insensitive to external disturbances and model uncertainties, and the effectiveness of SE is proved in the second simulation.
نوع الوثيقة: article
وصف الملف: electronic resource
اللغة: English
تدمد: 2226-4310
Relation: https://www.mdpi.com/2226-4310/9/7/352; https://doaj.org/toc/2226-4310
DOI: 10.3390/aerospace9070352
URL الوصول: https://doaj.org/article/cf21cb4effa14a44b558b69a82aabf53
رقم الانضمام: edsdoj.f21cb4effa14a44b558b69a82aabf53
قاعدة البيانات: Directory of Open Access Journals
الوصف
تدمد:22264310
DOI:10.3390/aerospace9070352