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

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书目名称Aerospace Mechatronics and Control Technology影响因子(影响力)




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书目名称Aerospace Mechatronics and Control Technology读者反馈学科排名

Indigence

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

Abrade

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

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

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

pulmonary-edema

绝缘

intuition