Plug and Play Robust Distributed Control with Ellipsoidal Parametric Uncertainty System by Hong Wang-jian, Wang Yan-xiang

“…Finally by one example of aircraft flutter model parameter identification, the efficiency of the proposed control strategy can be easily realized.…”
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Main directions of implementing research results of artificial intelligence systems into domestic production by F. F. Sharipov, M. A. Dyakonova

“…Wireless communication, the Internet of Things, unmanned vehicle including aircraft are the terms of the XXI century. The purpose of the study is to define the theoretical principles of digitalization in the manufacturing process for those who are interested in this issue. …”
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Influence of Fluid on Seal and Assembly of Pipeline Fittings Based on the Multiscale Finite Element Model by Yangyang Yan, Yaping Fan

“…Pipeline fittings with ferrules are applied to connect sections of hydraulic pipelines in aircraft, and their reliability and stability are essential. …”
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Control of Energy Storage Systems for Aeronautic Applications by G. Canciello, A. Cavallo, B. Guida

“…Future aircraft will make more and more use of automated electric power system management onboard. …”
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A Comparative Design and Analysis of Conventional and Variable Connecting Rod of Engines by Timur Choban Khidir, Bilal Mohammed Qasim, Ahmed Yashar, Burak Sahin

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Efficient Method for Aeroelastic Tailoring of Composite Wing to Minimize Gust Response by Yang Yu, Zhengjie Wang, Shijun Guo

“…This method has been applied to the aeroelastic tailoring of a composite wing of a tailless aircraft for minimum gust response. The results have shown that 20%–36% gust response reduction has been achieved for this case. …”
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Research on Complex Multiconstraint Path Planning Based on ACA Hybrid Algorithm by Hongyun Wang, Min Gao, Weiwei Gao, Wenzhao Li

“…According to the actual aircraft, a multiconstrained path cost model with seven components is constructed and defined the parameters and penalty factors of each part. …”
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A method and apparatus for inspecting large flat composite parts by using the Infrared LST technique by Vladimir Vavilov, Arsenii Chulkov, Denis Nesteruk, Douglas Burleigh, Alexey Moskovchenko

“… The principle of Line Scan Thermography (LST) was used to develop a self-propelled infrared thermographic nondestructive testing device for the inspection of large, relatively flat composite aerospace parts, such as aircraft wings. The design of the unit allowed the suppression of noise from reflected radiation. …”
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The Use of Drones in Emergency Medicine: Practical and Legal Aspects by Anna Konert, Jacek Smereka, Lukasz Szarpak

“…One must, however, be aware of the existing regulations regarding drone flights as an appearance of an unreported unmanned aircraft in the controlled space is identified worldwide as affecting aviation safety.…”
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A Preliminary Research on Combustion Characteristics of a Novel-Type Scramjet Combustor by Linqing Zhang, Juntao Chang, Wenxiang Cai, Hui Sun, Yingkun Li

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Study on Identification Method for Parameter Uncertainty Model of Aero Engine by Jie Bai, Shuai Liu, Wei Wang

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Design of Reduced-Order Multiple Observers for Uncertain Systems with Unknown Inputs by Mihai Lungu

“…To validate the suggested design algorithm, the steps of the design procedure have been summarized and software implemented for the concrete case of a light aircraft lateral-directional motion.…”
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Experimental Investigation into the Control and Load Alleviation Capabilities of Articulated Winglets by A. Gatto, P. Bourdin, M. I. Friswell

“…The philosophy of the concept centres around the use of active, in-flight adjustment of each wing's winglet dihedral angle, both as a primary means of aircraft roll control (single winglet actuation) and though smaller equal and simultaneous winglet deflections, tailor and alleviate main wing load. …”
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Vision-Based Tracking of Uncooperative Targets by Suresh K. Kannan, Eric N. Johnson, Yoko Watanabe, Ramachandra Sattigeri

“…The problem of a follower aircraft tracking an uncooperative leader, using vision information only, is addressed. …”
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Influence of External Factors on Airborne Missile’s Horizontal Backward Launching by Xiao Pan, Yi Jiang, Dong Hu, Huihui Guan

“…This paper studies the influence of different external disturbance factors on the horizontal backward separation of airborne missiles on large transport aircraft. The method of comparison with experiment was adopted to verify the accuracy of the finite element model during the ejection process. …”
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Research on Forecasting of the Compressor Geometric Variable System Based on the MAE Model by Cunjiang Xia, Yuyou Zhan, Yan Tan, Wenqing Wu

“…Unlike previous studies that used simulated or lab-generated data, we use actual flight data recorded by the aircraft data acquisition system to make our results more realistic. …”
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Mobile Multi-Agent Evaluation Method for Wireless Sensor Networks-Based Large-Scale Structural Health Monitoring by Shenfang Yuan, Dong Liang, Lei Qiu, Menglong Liu

“…Wireless sensor networks are increasingly adopted both in aircraft and civil structural health monitoring. However, due to the limited resources on a wireless sensor node, structural evaluation ability of the wireless sensor network is also limited, especially for large-scale structures. …”
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Stability Analysis of Pneumatic Cabin Pressure Regulating System with Complex Nonlinear Characteristics by Xinhua Zheng, Lili Xie, Lizhuo Liu

“…Phase plane analysis shows that there exists a limit cycle, which is responsible for pressure pulsating in aircraft cabin. After parameters adjustment, excellent stability characteristics are acquired. …”
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Feasibility of Hydrogen Energy for High-Power Aerospace Applications: A Comprehensive Assessment by Cai Zhenglin

“…The analysis focuses on fuel efficiency gains, emission reductions, and the integration of hydrogen-powered aircraft into current systems. Considerations include structural design, aerodynamic characteristics, weight distribution, refueling infrastructure, and regulatory compliance. …”
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Visual Explainable Convolutional Neural Network for Aerodynamic Coefficient Prediction by Yanxuan Zhao, Chengwen Zhong, Fang Wang, Yueqing Wang

“…Recently, aerodynamic performance analysis has been widely studied due to its importance in aircraft design. Most works adopted computational fluid dynamics (CFD) simulation to compute the aerodynamic forces, which is time consuming. …”
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