评估
发表于 2025-3-21 17:13:00
书目名称Aerospace Mechatronics and Control Technology影响因子(影响力)<br> http://figure.impactfactor.cn/if/?ISSN=BK0150529<br><br> <br><br>书目名称Aerospace Mechatronics and Control Technology影响因子(影响力)学科排名<br> http://figure.impactfactor.cn/ifr/?ISSN=BK0150529<br><br> <br><br>书目名称Aerospace Mechatronics and Control Technology网络公开度<br> http://figure.impactfactor.cn/at/?ISSN=BK0150529<br><br> <br><br>书目名称Aerospace Mechatronics and Control Technology网络公开度学科排名<br> http://figure.impactfactor.cn/atr/?ISSN=BK0150529<br><br> <br><br>书目名称Aerospace Mechatronics and Control Technology被引频次<br> http://figure.impactfactor.cn/tc/?ISSN=BK0150529<br><br> <br><br>书目名称Aerospace Mechatronics and Control Technology被引频次学科排名<br> http://figure.impactfactor.cn/tcr/?ISSN=BK0150529<br><br> <br><br>书目名称Aerospace Mechatronics and Control Technology年度引用<br> http://figure.impactfactor.cn/ii/?ISSN=BK0150529<br><br> <br><br>书目名称Aerospace Mechatronics and Control Technology年度引用学科排名<br> http://figure.impactfactor.cn/iir/?ISSN=BK0150529<br><br> <br><br>书目名称Aerospace Mechatronics and Control Technology读者反馈<br> http://figure.impactfactor.cn/5y/?ISSN=BK0150529<br><br> <br><br>书目名称Aerospace Mechatronics and Control Technology读者反馈学科排名<br> http://figure.impactfactor.cn/5yr/?ISSN=BK0150529<br><br> <br><br>
Indigence
发表于 2025-3-21 22:24:41
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
命令变成大炮
发表于 2025-3-22 03:13:51
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Abrade
发表于 2025-3-22 06:10:54
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
Hemiplegia
发表于 2025-3-22 10:18:09
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
glisten
发表于 2025-3-22 15:55:55
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
Interlocking
发表于 2025-3-22 17:24:58
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pulmonary-edema
发表于 2025-3-23 00:00:22
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绝缘
发表于 2025-3-23 04:47:00
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intuition
发表于 2025-3-23 06:20:54
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