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

激怒某人

978-981-16-6642-1The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapor

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Fulsome

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Numerical Study on Aerodynamic Performance of Hypersonic Vehicle with Aerospikess on the aerospike’s . ratios. Among the different aerospike configurations studied, the drag reduction effect of aerospike when the .?=?1 is the best, and the maximum value of the drag reduction efficiency is 36.4%. Within the scope of this study, as the . ratio of the aerospike increases, the drag

NAUT

Terminal Multi-Constrained Finite Time Sliding Mode Guidance Law Based on Truncation Function for Hyees of freedom in the transverse plane to ensure the constraint of impact velocity. The simulation verified that the guidance method can meet the requirements of terminal multiple constraints of hypersonic vehicle.

cunning

hyperuricemia

Dynamic Detection Method for Blade Tip Clearance of Aero-Engine in Assembled State Based on Linear Sa. Compared to the traditional methods, the BTC in whole circumferential phase can be measured rather than single phase. Meanwhile, the proposed method is not influenced by casing deformation and installation errors. Finally, the feasibility and capability of the system is verified by simulation exp

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過分自信

Design and Optimization of the Flexible Support Structure for Space Mirrorflexure hinges were established aiming at maintaining high static precision of the mirror under multi-conditions, and the resilient connector was optimized by stress deconcentration and viscoelastic materials damping to obtain adequate dynamic strength margin. Finally, the comprehensive performance

陰謀小團體

Target Localization on Image-Guided Missilecoordinate system. The proposed method is validated in the flight data of a certain type of image-guided missile, and a high-precision localization result is obtained at a long missile-target distance.