Improving aircraft performance using machine learning a review Soledad Le Clainche1 Esteban Ferrer1 Sam Gibson2 Elisabeth Cross2 Alessandro Parente3 Ricardo Vinuesa4

2025-05-08 0 0 1.92MB 56 页 10玖币
侵权投诉
Improving aircraft performance using machine learning: a review
Soledad Le Clainche1, Esteban Ferrer1, Sam Gibson2,
Elisabeth Cross2, Alessandro Parente3, Ricardo Vinuesa4
1Universidad Polit´
ecnica de Madrid, Spain
2University of Sheffield, United Kingdom
3Universit´
e Libre de Bruxelles, Belgium
4KTH Royal Institute of Technology, Sweden
Abstract
This review covers the new developments in machine learning (ML) that are impacting
the multi-disciplinary area of aerospace engineering, including fundamental fluid dynamics
(experimental and numerical), aerodynamics, acoustics, combustion and structural health
monitoring. We review the state of the art, gathering the advantages and challenges of ML
methods across different aerospace disciplines and provide our view on future opportunities.
The basic concepts and the most relevant strategies for ML are presented together with the
most relevant applications in aerospace engineering, revealing that ML is improving aircraft
performance and that these techniques will have a large impact in the near future.
Contents
1 Introduction 2
2 Machine learning methodology: a general overview 5
2.1 Neuralnetworks ...................................... 5
2.2 Regression and Classification . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
2.3 Semi-supervisedlearning ................................. 9
2.4 Unsupervised learning: clustering and dimensionality reduction . . . . . . . . . . 11
2.4.1 Clustering...................................... 11
2.4.2 Dimensionality reduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
2.4.3 Principal Component Analysis . . . . . . . . . . . . . . . . . . . . . . . . . . 12
2.4.4 Local dimensionality reduction . . . . . . . . . . . . . . . . . . . . . . . . . . 13
2.4.5 KernelPCA ..................................... 14
2.4.6 Autoencoders.................................... 14
3 Fluid mechanics 14
3.1 Computational fluid dynamics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
3.2 Reduced-ordermodels................................... 16
3.3 Experiments......................................... 18
4 Aerodynamics 19
4.1 Aerodynamic coefficients estimation . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
4.2 Aeroelasticity ........................................ 21
4.3 Designoptimization .................................... 22
Corresponding author: XX
1
arXiv:2210.11481v1 [cs.LG] 20 Oct 2022
5 Aeroacoustics 23
6 Combustion 25
6.1 Data analysis and feature extraction . . . . . . . . . . . . . . . . . . . . . . . . . . . 25
6.2 Dimensionality reduction, classification and adaptive chemistry . . . . . . . . . . . 26
6.3 Combustionclosures .................................... 27
6.4 Reduced-order models for realistic combustion systems . . . . . . . . . . . . . . . . 28
7 Structural assessment 29
8 Conclusions 31
1 Introduction
Climate change and increasing resource scarcity are challenges that Europe needs to face in the
coming decades. All this has a direct impact on air transport, which is struggling to maintain its
performance and competitiveness while ensuring a development focused on sustainable mobil-
ity. Research and innovation are essential to maintain the capabilities of the aviation industry,
driven by the rise of new markets and new competitors as a result of globalization. A new long-
term vision for the aeronautics sector is essential to ensure its successful advancement. In this
line, new requirements for the future aviation industry have been defined by the ACARE Flight-
path 2050, a Group of Recognized Personalities in the aeronautic sector, including stakeholders
from the aeronautics industry, air traffic management, airports, airlines, energy providers and
the research community. Aeronautics and air transport comprises both: air vehicle and system
technology. The future of aviation should focus on improving design, reducing manufactur-
ing time and cost (including certification and upgrade processes), and also improving the parts
forming the overall air travel system (general aviation, aircraft, airlines, airports, air traffic man-
agement and maintenance, repair and overhaul).
The ACARE Flightpath 2050 has defined 5 goals that should be achieved by 2050 to guarantee
the path through sustainable mobility:
Compared to the capabilities of a typical aircraft in the year 2000, by 2050 new technolo-
gies should allow 90% reduction in NOx emissions, 75% reduction in CO2 emissions per
passenger/kilometre and 65% reduction in noise emission of flying aircraft.
When taxiing, aircraft movements should be emission-free.
Novel strategies to design and manufacture aerial vehicles should be developed to make
them recyclable.
Sustainable alternative fuels should be developed to position Europe as the centre of excel-
lence in the field, and sustained by a strong European energy policy.
By 2025, Europe should take the lead to establish global environmental standards, formu-
lating and prioritizing an environmental action plan, and being at the forefront of atmo-
spheric research.
At the same time, ensuring safety and security is also a major priority, with the aim at reducing
by 80% the number of accidents by 2050 compared to 2000, taking into account the rising traffic.
2
To achieve these goals, it is extremely important to find newer eco-friendly alternatives suit-
able for the industry to reduce the aviation net carbon emissions and noise. To this aim, the
aerospace industry is gathering efforts towards developing new aerodynamic designs, more ef-
ficient, reducing the oil consumption whilst maintaining the safety in the flight performance.
Moreover, finding new alternatives to fossil fuels, improving the energy efficiency in combus-
tion systems, or finding optimal routes for air traffic management (ATM) are also some of the key
points where the aerospace industry should advance to minimize the environmental footprint.
However, to achieve these objectives it is not enough to improve the ‘standard’ configurations.
The aerospace engineering industry is aware that to go beyond the state-of-the-art it is necessary
to develop novel ground-breaking disruptive technologies.
Fluid and solid mechanics need to be advanced with applications in aerodynamics, acoustics,
and combustion, to develop new technologies, resulting in novel aircraft designs with reduced
environmental impact (see Fig. 1). Researchers in collaboration with the aeronautical industry
should explore: (i) new aircraft configurations able to reduce noise and pollution emissions, (ii)
cruise drag reduction by manipulating turbulent flow structures close to the aircraft surface (i.e.,
delaying the boundary transition from laminar to turbulent flow), using novel friendly low-risk
practices, (iii) novel strategies for flow control (rising the benefits achieved by only changing the
external shape) to enhance the aerodynamic performance reducing drag, noise or flow transition,
rising lift or controlling unsteadiness or flow separation, and (iv) reduce the system complexity
with novel aircraft materials and lighter designs (which directly results in less fuel consump-
tion), and reduced aircraft maintenance and life cost cycle [3].
Figure 1: Towards sustainable aviation using machine learning.
High-fidelity numerical simulations and advanced experimental techniques (i.e., wind tunnel
experiments or open-air experiments as in the case of flight test, et cetera) allow collecting a
large variety of data, containing relevant information about physical principles connected to
the aerodynamic performance of the aircraft, the efficiency of the combustion system or the
main instabilities driving the flow dynamics and the possibility of attenuating or boosting such
instabilities using active or passive flow control techniques [2]. Additionally, experiments (i.e.,
ultrasounds, non-intrusive testing, et cetera) and simulations provide information connected
to the fundamentals of solid mechanics, the presence of noise and the structural health of the
aircraft, allowing for noise control and early failure detection.
3
However, the economic and computational cost, related to the performance of experiments
and simulations, encourages researchers to look for new alternatives, which allow to advance
in the field i.e., developing relevant technologies for the aerospace industry, while avoiding de-
lays in the manufacturing and time-to-market process. Aircraft development, manufacturing,
maintenance and support are four critical levels that must be accurate and reliable to ensure the
success of the aerospace industry.
Artificial intelligence (AI) and machine learning (ML) have been introduced in the aerospace
industry for various applications connected to the reduction of aircraft’s environmental impact,
including data interpretation [174], system management, customer service or aircraft modelling
and to generate new high-fidelity databases at a reduced (economic and CPU) cost [191], solving
problems of optimization, flow control, or even providing optimal sensors distributions for solid
mechanics or aeroelasticity applications. In the recent review article by Brunton et al. [40], the
authors summarize the new trends and perspective of ML in the aerospace industry, including
its application for smart manufacturing, and in the development (and aircraft design), produc-
tion and product support phases (aircraft design, manufacturing, verification and validation).
The authors reveals the possibilities of ML to process data in light computations increasing the
production rate, based on the idea of the use of ML techniques that are measurable, interpretable
and certifiable.
ML is generally understood as a branch of AI, although there are nuances in the definition:
ML aims at improving systems performance using self-learning algorithms, while AI tries to
mimic natural intelligence solving complex problems and enabling decision making (although
not maximizing the system efficiency) [242]. Both AI and ML are connected to Big Data, a term
that linked to the enormous volume of data that floods the aeronautical sector every day or that
is generated from CFD simulations or experimental measurements and connected to aircraft
aerodynamic performance [62, 216]. Combining Big Data with ML techniques, it is possible to
develop reduced dimensional systems, such as reduced order models (ROMs) [171, 318], capable
to accurately predict the evolution of the flow dynamics [2, 110, 172] (i.e., flow control, reduce
cruise drag [295], boundary layer transition, etc.), or surrogate models, capable to predict the
aerodynamic forces and moments acting on the aircraft as a function of some parameters (i.e.,
Reynolds number, Mach number, geometry shape, etc.).
This review provides a state-of-the-art of AI and ML applications in the aerospace engineer-
ing field. The basic concepts and most relevant strategies for ML and AI are brought together to
explain the similarities found in the nomenclature of similar techniques used in different fields,
also shedding light on new applications of these algorithms, quite extended in other fields but
not known to the aerospace industry. For example, the review details the use of machine learning
for reduced order modelling, which can be used to accelerate numerical simulations, or for tem-
poral and spatial forecast (including non-intrusive sensing). Additionally, we include relevant
applications of the field, including flow control, acoustics, combustion, flight test and structural
health monitoring.
This article intends to explore the possibilities of ML, an emerging field for the aerospace in-
dustry, identifying new research lines of potential interest and bringing new ideas to developing
the technologies of the future, and founded on a primary goal: to fight climate change. This ar-
ticle reviews the main disciplines connected to the aerodynamic performance of the aircraft (see
Fig. 1): fundamental fluid dynamics, aerodynamics, acoustics, combustion, and general solid
mechanics; and based on the idea of finding novel efficient designs, capable to reduce noise and
pollutant emissions, while at the same time, ensuring safety and security.
The article is organized as follows. Section 2 introduces the machine learning methodologies,
4
and the literature review of the main applications in aerospace engineering is presented in Sec-
tion 3 for fundamental fluid dynamics, Section 4 for aerodynamics, Section 5 for aeroacoustics,
Section 6 for combustion and Section 7 for solid mechanics. The main conclusions are presented
in Section 8.
2 Machine learning methodology: a general overview
Current advances in computer science are strongly related to the increasing amount of data gen-
erated and stored in the different disciplines conforming aerospace engineering. The valuable
information contained in these databases encourages researchers to develop and test sophisti-
cated algorithms to exploit such information, to gain insight and knowledge from the data and
to subsequently propose and develop new commercial strategies aligned with the ideas behind
the concept of sustainable aviation: developing new cleaner and safer aircraft designs. ML is a
fast-growing science in the field of aerospace engineering due to its good capabilities to extract
information from complex databases, which it later used to develop models, such as ROMs or
surrogate models. Based on available data and the type of training carried out within the analy-
sis, ML algorithms can be classified into unsupervised, semi-supervised or supervised learning,
as presented in Fig. 2. This section briefly introduces the basic idea behind some of these ML al-
gorithms, which have been used for different applications in the field of aerospace engineering.
Figure 2: Machine learning methods: a general overview. Classification extracted from Ref. [39].
In bold, the most popular techniques in the field of aerospace engineering.
2.1 Neural networks
ML uses artificial neural networks (ANNs), also called as neural networks (NNs), to process
and extract information from databases. The name of this computing system is inspired by the
biological neural networks of the human brain. ML uses NNs to solve an optimization prob-
lem. More specifically, using back propagation and stochastic gradient descent algorithms, ML
optimizes the following compound function
arg min
Aj
(fP(AP,··· , f2(A2, f1(A1,X)) ···) + λg(Aj)),(1)
5
摘要:

Improvingaircraftperformanceusingmachinelearning:areviewSoledadLeClainche1,EstebanFerrer1,SamGibson2,ElisabethCross2,AlessandroParente3,RicardoVinuesa41UniversidadPolit´ecnicadeMadrid,Spain2UniversityofShefeld,UnitedKingdom3Universit´eLibredeBruxelles,Belgium4KTHRoyalInstituteofTechnology,SwedenAbs...

展开>> 收起<<
Improving aircraft performance using machine learning a review Soledad Le Clainche1 Esteban Ferrer1 Sam Gibson2 Elisabeth Cross2 Alessandro Parente3 Ricardo Vinuesa4.pdf

共56页,预览5页

还剩页未读, 继续阅读

声明:本站为文档C2C交易模式,即用户上传的文档直接被用户下载,本站只是中间服务平台,本站所有文档下载所得的收益归上传人(含作者)所有。玖贝云文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。若文档所含内容侵犯了您的版权或隐私,请立即通知玖贝云文库,我们立即给予删除!
分类:图书资源 价格:10玖币 属性:56 页 大小:1.92MB 格式:PDF 时间:2025-05-08

开通VIP享超值会员特权

  • 多端同步记录
  • 高速下载文档
  • 免费文档工具
  • 分享文档赚钱
  • 每日登录抽奖
  • 优质衍生服务
/ 56
客服
关注