Sparse online Gaussian process regression-based robust nonlinear dynamic inversion for multirotor with forward flight ground effect

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Jayden Dongwoo Lee, Youngjae Kim, Lamsu Kim, Natnael S. Zewge, Hyochoong Bang
{"title":"Sparse online Gaussian process regression-based robust nonlinear dynamic inversion for multirotor with forward flight ground effect","authors":"Jayden Dongwoo Lee,&nbsp;Youngjae Kim,&nbsp;Lamsu Kim,&nbsp;Natnael S. Zewge,&nbsp;Hyochoong Bang","doi":"10.1016/j.ast.2025.110195","DOIUrl":null,"url":null,"abstract":"<div><div>This paper proposes a sparse online Gaussian process-based robust nonlinear dynamic inversion (SOGPR-RNDI) to compensate for ground effect during forward flight. Ground effect is challenging to model as it varies with altitude, thrust, propeller radius, platform movement, and surface quality. Its characteristics change significantly during forward flight due to aerodynamic effects. To address this problem, sparse online Gaussian process regression (SOGPR), a non-parametric modeling method, is employed to estimate and compensate for ground effect in real-time. SOGPR updates the mean and variance through a recursive process and uses a kernel linear independence test to maintain a meaningful dataset while reducing a computational burden. The proposed controller integrates a baseline control input, a Gaussian process regression (GPR) control input, and a robust control input, which is designed using the time derivative of the uncertainty error to ensure tracking performance and mitigate chattering issues. In addition, finite-time asymptotic convergence of the closed-loop system is proved using Lyapunov stability. Simulation results demonstrate that the proposed method effectively compensates for ground effect during forward flight and achieves superior tracking performance compared to nonlinear disturbance observer (NDO), deep neural network (DNN), modified GPR (MGPR), and SOGPR-based nonlinear dynamic inversion (SOGPR-NDI). Notably, SOGPR-RNDI reduces altitude root mean square error (RMSE) by 18.7% and velocity RMSE by 12.4% compared to SOGPR-NDI. Moreover, the computational efficiency of SOGPR-RNDI is analyzed, demonstrating its real-time applicability through better training and execution times compared to other methods.</div></div>","PeriodicalId":50955,"journal":{"name":"Aerospace Science and Technology","volume":"162 ","pages":"Article 110195"},"PeriodicalIF":5.0000,"publicationDate":"2025-04-09","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Science and Technology","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1270963825002664","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

Abstract

This paper proposes a sparse online Gaussian process-based robust nonlinear dynamic inversion (SOGPR-RNDI) to compensate for ground effect during forward flight. Ground effect is challenging to model as it varies with altitude, thrust, propeller radius, platform movement, and surface quality. Its characteristics change significantly during forward flight due to aerodynamic effects. To address this problem, sparse online Gaussian process regression (SOGPR), a non-parametric modeling method, is employed to estimate and compensate for ground effect in real-time. SOGPR updates the mean and variance through a recursive process and uses a kernel linear independence test to maintain a meaningful dataset while reducing a computational burden. The proposed controller integrates a baseline control input, a Gaussian process regression (GPR) control input, and a robust control input, which is designed using the time derivative of the uncertainty error to ensure tracking performance and mitigate chattering issues. In addition, finite-time asymptotic convergence of the closed-loop system is proved using Lyapunov stability. Simulation results demonstrate that the proposed method effectively compensates for ground effect during forward flight and achieves superior tracking performance compared to nonlinear disturbance observer (NDO), deep neural network (DNN), modified GPR (MGPR), and SOGPR-based nonlinear dynamic inversion (SOGPR-NDI). Notably, SOGPR-RNDI reduces altitude root mean square error (RMSE) by 18.7% and velocity RMSE by 12.4% compared to SOGPR-NDI. Moreover, the computational efficiency of SOGPR-RNDI is analyzed, demonstrating its real-time applicability through better training and execution times compared to other methods.

Abstract Image

基于稀疏在线高斯过程回归的多旋翼前飞地面效应鲁棒非线性动态反演
本文提出了一种基于稀疏在线高斯过程的鲁棒非线性动态反演方法(SOGPR-RNDI)来补偿前飞过程中的地面效应。由于地面效应随高度、推力、螺旋桨半径、平台运动和地面质量的变化而变化,因此地面效应的建模具有挑战性。在前飞过程中,由于空气动力学的影响,其特性发生了显著变化。为了解决这一问题,采用稀疏在线高斯过程回归(SOGPR)这种非参数建模方法对地面效应进行实时估计和补偿。SOGPR通过递归过程更新均值和方差,并使用核线性独立性测试来维护有意义的数据集,同时减少计算负担。该控制器集成了基线控制输入、高斯过程回归(GPR)控制输入和鲁棒控制输入,并利用不确定性误差的时间导数设计鲁棒控制输入,以确保跟踪性能并减轻抖振问题。此外,利用Lyapunov稳定性证明了闭环系统的有限时间渐近收敛性。仿真结果表明,与非线性扰动观测器(NDO)、深度神经网络(DNN)、修正GPR (MGPR)和基于sogpr的非线性动态反演(SOGPR-NDI)相比,该方法有效地补偿了前飞过程中的地面效应,取得了更好的跟踪性能。值得注意的是,与SOGPR-NDI相比,SOGPR-RNDI将海拔均方根误差(RMSE)降低了18.7%,速度均方根误差(RMSE)降低了12.4%。分析了SOGPR-RNDI算法的计算效率,通过提高训练次数和执行次数,证明了其实时性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信