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Titlebook: Aerospace Mechatronics and Control Technology; Selected Contributio Huafeng Ding Conference proceedings 2022 The Editor(s) (if applicable)

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發(fā)表于 2025-3-21 17:13:00 | 只看該作者 |倒序瀏覽 |閱讀模式
期刊全稱Aerospace Mechatronics and Control Technology
期刊簡稱Selected Contributio
影響因子2023Huafeng Ding
視頻videohttp://file.papertrans.cn/151/150529/150529.mp4
發(fā)行地址Presents the latest trends and advances in mechanical engineering and aerospace engineering.Makes valuable contributions to academic researchers and engineers in the industry.Collects chapters as sele
學(xué)科分類Springer Aerospace Technology
圖書封面Titlebook: Aerospace Mechatronics and Control Technology; Selected Contributio Huafeng Ding Conference proceedings 2022 The Editor(s) (if applicable)
影響因子This book collects chapters on Aerospace Mechatronics and Control Technology as selected contributions from the 7th Asia Conference on Mechanical Engineering and Aerospace Engineering (MEAE) in 2021. The book focuses on novel techniques for aviation infrastructure in aerospace mechatronics and avionics systems, mechanical engineering in aerospace, and mechanical design and control system domains. The contents make valuable contributions to academic researchers and engineers in the industry..The MEAE 2021 provides a forum to discuss the latest trends and advances in mechanical engineering and aerospace engineering and related fields, and foster the exchange of ideas and international collaboration in the field..
Pindex Conference proceedings 2022
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書目名稱Aerospace Mechatronics and Control Technology影響因子(影響力)




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Terminal Multi-Constrained Finite Time Sliding Mode Guidance Law Based on Truncation Function for Hyocity was studied. Firstly, a finite time sliding mode control method based on truncation function for second order nonlinear system was proposed, and then a reasonable truncation function was designed according to the dynamic equation of the terminal guidance phase of the vehicle to form the slidin
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DSMC Study for Effects of Angles of Attack on Closed Cavity of Space Vehicle in Hypersonic Rarefied pace vehicles in rarefied gas flow, Direct Simulation Monte Carlo method (DSMC) with the adaptive grid is used. The free stream at a Mach Number of 8, an altitude of 60?km, and the angles of attack (AOA) ranging from 0° to 60°.The results show that the closed cavity changes its type when AOA changes
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The Cause and Effect Analysis of Aero-Engine Roller Bearing Skid Based on Assembly Process Inspectiocess, practical use, trial run, measurement and inspection by fishbone diagram. In order to ensure the economy and airworthiness of aero-engine manufacturing, the use and repair of bearing with skid damage were discussed by means of information statistics and trial run experiments. Then the effect o
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Dynamic Detection Method for Blade Tip Clearance of Aero-Engine in Assembled State Based on Linear Sl inspection indicator during engine assembly. With the higher demand for consistency of engine performance, the measurability of BTC is required to be much more accurate and dynamically. However, the traditional BTC detection method in the assembly process is restricted to lower accuracy, inability
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