標(biāo)題: Titlebook: Aerospace Mechatronics and Control Technology; Selected Contributio Huafeng Ding Conference proceedings 2022 The Editor(s) (if applicable) [打印本頁(yè)] 作者: 評(píng)估 時(shí)間: 2025-3-21 17:13
書目名稱Aerospace Mechatronics and Control Technology影響因子(影響力)
書目名稱Aerospace Mechatronics and Control Technology影響因子(影響力)學(xué)科排名
書目名稱Aerospace Mechatronics and Control Technology網(wǎng)絡(luò)公開度
書目名稱Aerospace Mechatronics and Control Technology網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Aerospace Mechatronics and Control Technology被引頻次
書目名稱Aerospace Mechatronics and Control Technology被引頻次學(xué)科排名
書目名稱Aerospace Mechatronics and Control Technology年度引用
書目名稱Aerospace Mechatronics and Control Technology年度引用學(xué)科排名
書目名稱Aerospace Mechatronics and Control Technology讀者反饋
書目名稱Aerospace Mechatronics and Control Technology讀者反饋學(xué)科排名
作者: Indigence 時(shí)間: 2025-3-21 22:24
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作者: 命令變成大炮 時(shí)間: 2025-3-22 03:13 作者: Abrade 時(shí)間: 2025-3-22 06:10
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作者: Hemiplegia 時(shí)間: 2025-3-22 10:18
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作者: glisten 時(shí)間: 2025-3-22 15:55
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作者: Interlocking 時(shí)間: 2025-3-22 17:24 作者: pulmonary-edema 時(shí)間: 2025-3-23 00:00 作者: 絕緣 時(shí)間: 2025-3-23 04:47 作者: intuition 時(shí)間: 2025-3-23 06:20 作者: Traumatic-Grief 時(shí)間: 2025-3-23 09:47
Experimental Research on the Influence of the Bulk Swirl on the Compressorcompressor characteristic experiment under the overall vortex flow distortion generator based on the overall vortex flow distortion generator, and measured the performance of the swirl flow distortion generator. The generated swirl field obtains the pressure ratio and efficiency characteristics of t作者: 混合物 時(shí)間: 2025-3-23 14:22
Target Localization on Image-Guided Missilea target localization method that combines on-board IMU data and image information. This method does not require equipment such as GPS or optoelectronic platform, nor does it need prior knowledge or templates of the target. Firstly, a selection strategy is proposed to determine keyframes, which are 作者: Leisureliness 時(shí)間: 2025-3-23 19:06
Attitude Updating Algorithm Based on Agile Micro-Nano Satellites attitude updating algorithm of the traditional micro-nano satellite is no longer applicable. This paper proposes a modified attitude updating scheme applied to agile satellites. The method adopts the coning motion as the research scene, in which the influence of noncommutativity error is the worst.作者: lethal 時(shí)間: 2025-3-24 01:34 作者: 歹徒 時(shí)間: 2025-3-24 04:15 作者: CANT 時(shí)間: 2025-3-24 09:55
Simona Pekarek Doehler,Evelyne Berger flow around the blunt body with aerospike are investigated for the aerospike’s changing . ratios with freedom Mach number of 5.75. The effect of the characteristics of the flow field and the aerospike’s . ratios on the drag coefficient of model and the surface pressure coefficient of the nose cone 作者: Latency 時(shí)間: 2025-3-24 13:27 作者: atrophy 時(shí)間: 2025-3-24 16:49
https://doi.org/10.1007/978-3-030-22165-2t, the time domain and frequency domain identification should be carried out by measuring the performance indexes of the air rudder, which is used for the 6-DOF simulation of the aircraft. This paper designs the test platform and test scheme of the air rudder of the boost glide aircraft, and tests t作者: 檢查 時(shí)間: 2025-3-24 22:14 作者: gastritis 時(shí)間: 2025-3-24 23:34
Simona Pekarek Doehler,Evelyne Bergercess, 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作者: discord 時(shí)間: 2025-3-25 07:19
End-to-End Neural Dialogue Systems,l 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作者: ACTIN 時(shí)間: 2025-3-25 07:47
Statistical Data-Driven Dialogue Systems,athematical model based analysis methods are studied to realize assembly deviation prediction. However, most established analysis methods require abstraction and simplification of geometric deviations, which results in the inability to accurately characterizing the surface deviation features and ana作者: 侵害 時(shí)間: 2025-3-25 13:54
Kei Wakabayashi,Johane Takeuchi,Mikio Nakanoproposes a method for online identification and prediction of solid rocket motor performance. The calculation model of the nozzle throat diameter and the propellant burning rate are established based on the analysis of internal correlation between motor parameters. Then by means of the real-time mea作者: Genistein 時(shí)間: 2025-3-25 18:33 作者: Cabinet 時(shí)間: 2025-3-25 23:30
https://doi.org/10.1007/978-981-19-5538-9 crucial importance to the system’s imaging quality. However, the mirror shape is usually influenced by gravity, temperature, forced displacement and launch vibrations to distort after leaving earth. The support structure of the subassembly plays an important role to minimize the impact of above fac作者: facetious 時(shí)間: 2025-3-26 01:27 作者: 破布 時(shí)間: 2025-3-26 07:29
Svetlana Stoyanchev,Stefan Ultes,Haizhou Lia target localization method that combines on-board IMU data and image information. This method does not require equipment such as GPS or optoelectronic platform, nor does it need prior knowledge or templates of the target. Firstly, a selection strategy is proposed to determine keyframes, which are 作者: ureter 時(shí)間: 2025-3-26 11:29
Learning to Rank Intents in Voice Assistants attitude updating algorithm of the traditional micro-nano satellite is no longer applicable. This paper proposes a modified attitude updating scheme applied to agile satellites. The method adopts the coning motion as the research scene, in which the influence of noncommutativity error is the worst.作者: 退出可食用 時(shí)間: 2025-3-26 14:37 作者: 滴注 時(shí)間: 2025-3-26 17:18
https://doi.org/10.1007/978-981-16-6640-7Aerospace Mechatronics; Mechanical Engineering; Mechanical Design; Control System; Fluid Mechanics and M作者: 激怒某人 時(shí)間: 2025-3-26 23:51
978-981-16-6642-1The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapor作者: 等待 時(shí)間: 2025-3-27 01:42 作者: Fulsome 時(shí)間: 2025-3-27 05:54 作者: 商品 時(shí)間: 2025-3-27 10:51
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作者: NAUT 時(shí)間: 2025-3-27 16:50
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.作者: cunning 時(shí)間: 2025-3-27 20:02 作者: hyperuricemia 時(shí)間: 2025-3-27 23:50
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作者: 有惡意 時(shí)間: 2025-3-28 03:39 作者: 過(guò)分自信 時(shí)間: 2025-3-28 10:15
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 作者: 陰謀小團(tuán)體 時(shí)間: 2025-3-28 11:47
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.作者: objection 時(shí)間: 2025-3-28 16:02 作者: 預(yù)知 時(shí)間: 2025-3-28 20:16 作者: ineptitude 時(shí)間: 2025-3-28 23:14
Simona Pekarek Doehler,Evelyne Bergers 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作者: Baffle 時(shí)間: 2025-3-29 05:15
Simona Pekarek Doehler,Evelyne Bergerees 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.作者: Epidural-Space 時(shí)間: 2025-3-29 10:05 作者: MUTE 時(shí)間: 2025-3-29 14:15
End-to-End Neural Dialogue Systems,a. 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作者: Iatrogenic 時(shí)間: 2025-3-29 18:02 作者: Incorruptible 時(shí)間: 2025-3-29 20:53
https://doi.org/10.1007/978-981-19-5538-9flexure 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 作者: 遺忘 時(shí)間: 2025-3-30 03:33 作者: 千篇一律 時(shí)間: 2025-3-30 04:11
Learning to Rank Intents in Voice Assistantsy. Finally, the rotation vector compensation algorithm is derived to gain the updating attitude. The proposed algorithm does not need equal interval angular velocity sampling and can achieve higher estimation accuracy in a dynamic environment than the traditional algorithms. The simulation results v作者: thalamus 時(shí)間: 2025-3-30 10:46
The Cause and Effect Analysis of Aero-Engine Roller Bearing Skid Based on Assembly Process Inspectioded. And the repair method, experimental content and inspection standard of bearing with skid are presented in detail. The research has important guiding significance for aero-engine bearing to master its working state, prevent its fault and guarantee the aviation safety.作者: chisel 時(shí)間: 2025-3-30 16:27
Conference proceedings 2022neering 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 academ作者: innovation 時(shí)間: 2025-3-30 20:27 作者: debunk 時(shí)間: 2025-3-30 21:01
