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Analytical models for the penetration of semi-infinite targets by rigid,deformable and erosive long rods 被引量:17
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作者 He-Ming Wen Bin Lan 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2010年第4期573-583,共11页
A theoretical study is presented herein on the pen- etration of a semi-infinite target by a spherical-headed long rod for Yp 〉 S, where Yp is the penetrator strength and S is the static target resistance. For Yp 〉 S... A theoretical study is presented herein on the pen- etration of a semi-infinite target by a spherical-headed long rod for Yp 〉 S, where Yp is the penetrator strength and S is the static target resistance. For Yp 〉 S, depending upon initial impact velocity, there exist three types of penetration, namely, penetration by a rigid long rod, penetration by a deforming non-erosive long rod and penetration by an erosive long rod. If the impact velocity of the penetrator is higher than the hydrodynamic velocity (VH), it will penetrate the target in an erosive mode; if the impact velocity lies between the hydrodynamic velocity (VH) and the rigid body velocity (VR), it will penetrate the target in a deformable mode; if the impact velocity is less than the rigid body velocity (VR), it will penetrate the target in a rigid mode. The critical conditions for the transition among these three penetration modes are proposed. It is demonstrated that the present model predictions correlate well with the experimental observations in terms of depth of penetration (DOP) and the critical transition conditions. 展开更多
关键词 Long rod Semi-infinite target - Penetration Alekseevskii-Tate model rigid body velocity - Hydrodynamic velocity
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Study of helicopter autorotation landing following engine failure based on a six-degree-of-freedom rigid-body dynamic model 被引量:12
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作者 Meng Wanli Chen Renliang 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2013年第6期1380-1388,共9页
This paper focuses on the prediction of the safe autorotation landing operations of a helicopter following engine failure.The autorotation landing procedure is formulated as a nonlinear optimal control problem based o... This paper focuses on the prediction of the safe autorotation landing operations of a helicopter following engine failure.The autorotation landing procedure is formulated as a nonlinear optimal control problem based on an augmented six-degree-of-freedom rigid-body flight dynamic model.First,the cost function and constraints are properly selected.The direct transcription approach is then employed to solve the optimal control problem.For a UH-60 helicopter,the optimal solutions with the rigid-body model are compared with those obtained using a two-dimensional point-mass model.It is found that the optimal solutions using the two different models show reasonably good agreement,and furthermore the optimal solutions using the rigid-body model involve the time histories of angular rates and attitudes,lateral velocity and position,as well as pitch controls.Finally the optimal control formulations with different cost functions are proposed for taking account of 1-s time delay and minimum touchdown speed.The calculated control strategies and trajectories are realistic. 展开更多
关键词 Autorotation landing Engine failure Helicopters Optimal control rigid-body model
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A 3-DOF Pseudo-Rigid-Body Model for Tension-Based Compliant Bistable Mechanisms 被引量:1
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作者 CHEN Guimin GAO Hongwei JIA Jianyuan 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2010年第2期149-153,共5页
Compliant bistable mechanisms, devices with two distinct stable equilibrium positions, are used in a variety of applications, such as switches, clasps, and valves. Many kinds of compliant bistable mechanisms were prop... Compliant bistable mechanisms, devices with two distinct stable equilibrium positions, are used in a variety of applications, such as switches, clasps, and valves. Many kinds of compliant bistable mechanisms were proposed and studied during the past decade. Among them, tension-based compliant bistable mechanisms, that incorporate tension pivots as their flexible members, feature in short travel distance and low power consuming. So far, the design of this kind of bistable mechanisms is done using finite element method through trial and error, thus is time-consuming. By treating the tension pivots as fixed-guided segments and their elongation as a spring, we developed a novel three degree-of-freedom (3-DOF) pseudo-rigid-body model (PRBM) for this kind of bistable mechanisms. The principle of virtual work is used to derive the force-deflection relationship of the PRBM model. The comparison between the PRBM results and the experimental results of the force-deflection characteristics shows that the PRBM can predict not only the bistable behavior of the tension-based bistable mechanisms, but also their soft spring-like post-bistable behavior and the spring-like force-deflection characteristics when pulling in the reverse direction from the as-fabricated position, which is called reverse behavior. The 3-DOF PRBM can be used to design and identify tension-based bistable mechanisms. Using the PRBM instead of the trial-and-error method can greatly reduce the development time of this kind of bistable mechanisms. 展开更多
关键词 compliant bistable mechanism pseudo-rigid-body model tension pivot
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Alternating Parity Band in Octupole-Soft ^(140)Xe with Axial Vibrational-Rotational Model and Triaxial Rigid Rotor Model
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作者 Xiao Lu Bin Qi Shou-Yu Wang 《Chinese Physics Letters》 SCIE CAS CSCD 2018年第10期9-13,共5页
Energies of the yrast positive-and negative-parity excited states in140 Xe are reproduced by two different models considering quadrupole-octupole deformations, namely the axial vibrational-rotational model and the tri... Energies of the yrast positive-and negative-parity excited states in140 Xe are reproduced by two different models considering quadrupole-octupole deformations, namely the axial vibrational-rotational model and the triaxial rigid rotor model, and compared with the stable octupole-deformed222 Th. The origin of the energy difference between the opposite parity sequences is considered from two different mechanisms, the vibration in axial deformed energy minima and the rotation considering the effective triaxial deformation. The success of reproducing the data in both the models implies that these two mechanisms are equivalent on some level for the octupole-soft nuclei. By investigating the probability distributions for projection of total angular momentum in the triaxial rigid rotor model, it is found that such an energy difference is associated with the difference of orientation of the rotational axis. 展开更多
关键词 Alternating Parity Band in Octupole-Soft Xe with Axial Vibrational-Rotational model and Triaxial rigid Rotor model
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Kinematic simulation of human gait with a multi-rigid-body foot model 被引量:2
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作者 YANG Yan HU Xiaochun LI Xiaopeng 《Computer Aided Drafting,Design and Manufacturing》 2012年第2期42-46,共5页
The paper builds a multi-rigid-body model of human with a 4-rigid-body foot in the 3D CAD software Solidworks, based on human anatomy. By controlling the rotation of the ankle and major joints of human body while walk... The paper builds a multi-rigid-body model of human with a 4-rigid-body foot in the 3D CAD software Solidworks, based on human anatomy. By controlling the rotation of the ankle and major joints of human body while walking, the Kinematic simulation was performed in the dynamics simulation software ADAMS. The paper analyzes the simulate results and points out deficiencies in the current work and the direction of research efforts in future. 展开更多
关键词 multi-rigid-body foot model human gait SIMULATION
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Dynamic model for landsliding monitoring under rigid body assumption
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作者 朱建军 丁晓利 陈永奇 《中国有色金属学会会刊:英文版》 CSCD 2001年第2期301-306,共6页
Based on the assumption that the slope bodies are rigid, the dynamic model of the landsiding (forward model) was put forward. According to the dynamic model, the system equations of Kalman filter were constituted. The... Based on the assumption that the slope bodies are rigid, the dynamic model of the landsiding (forward model) was put forward. According to the dynamic model, the system equations of Kalman filter were constituted. The mechanical status of a slope was hence combined with the monitoring data by Kalman filter. The model uncertainties or model errors could also be considered through some fictitious observation equations. Different from existed methods, the presented method can make use for not only the statistic information contained in the data but also the information provided by the mechanical and geological aspect of slopes. At last a numerical example was given out to show the feasibility of the method. [ 展开更多
关键词 dynamic model KALMAN filter rigid body LANDSLIDE MONITORING
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Non-rigid 3D models retrieval based on hierarchical matching
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作者 Liu Yujie Li Wei +3 位作者 Song Yang Gong Weiqing Li Zongmin Li Hua 《Computer Aided Drafting,Design and Manufacturing》 2017年第1期39-47,共9页
In 3D models retrieval, feature description and retrieval of non-rigid model face more complex problems due to the isometry transformation of itself. We introduce the hierarchical combination matching into the feature... In 3D models retrieval, feature description and retrieval of non-rigid model face more complex problems due to the isometry transformation of itself. We introduce the hierarchical combination matching into the feature comparison, and build a map between the divided regions of two models, and then achieve accurate feature matching based on patch-by-patch, which successfully introduces the spatial information into feature matching. Verified by experiment, the 3D model retrieval method proposed in this paper based on hierarchical combination matching can make sure more accurate feature matching, so as to enhance the precision of retrieval. 展开更多
关键词 non-rigid 3D model shape descriptor spatial distribution hierarchical combination matching
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A DYNAMIC MODEL FOR ROCKET LAUNCHER WITHCOUPLED RIGID AND FLEXIBLE MOTION
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作者 章定国 肖建强 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2005年第5期609-617,共9页
The dynamics of a coupled rigid-flexible rocket launcher is reported. The coupled rigid-flexible rocket launcher is divided into two subsystems, one is a system of rigid bodies, the other a flexible launch tube which ... The dynamics of a coupled rigid-flexible rocket launcher is reported. The coupled rigid-flexible rocket launcher is divided into two subsystems, one is a system of rigid bodies, the other a flexible launch tube which can undergo large overall motions spatially. First, the mathematical models for these two subsystems were established respectively. Then the dynamic model for the whole system was obtained by considering the coupling effect between these two subsystems. The approach, which divides a complex system into several simple subsystems first and then obtains the dynamic model for the whole system via combining the existing dynamic models for simple subsystems, can make the modeling procedure efficient and convenient. 展开更多
关键词 coupled rigid-flexible system rocket launcher dynamic modeling
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STATISTICAL MODELS FOR SEMI-RIGID NEMATIC POLYMERS
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作者 王新久 《Chinese Journal of Polymer Science》 SCIE CAS CSCD 1995年第4期361-365,共5页
Semi-rigid liquid crystal polymer is a class of liquid crystal polymers different from long rigid rod liquid crystal polymer to which the well-known Onsager and Flory theories are applied. In this paper, three statist... Semi-rigid liquid crystal polymer is a class of liquid crystal polymers different from long rigid rod liquid crystal polymer to which the well-known Onsager and Flory theories are applied. In this paper, three statistical models for the semi-rigid nematic polymer were addressed. They are the elastically jointed rod model, worm-like chain model, and non-homogeneous chain model. The nematic-isotropic transition temperature was examined. The pseudo-second transition temperature is expressed analytically. Comparisons with the experiments were made and the agreements were found. 展开更多
关键词 semi-rigid nematic polymer statistical model elastically-jointed rods worm-like chain non-homogeneous chain
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Reverse Monte Carlo Modeling of the Rigidity Percolation Threshold in Ge<SUB>x</SUB>Se<SUB>1-x</SUB>Glassy Networks
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作者 Moneeb T. M. Shatnawi 《New Journal of Glass and Ceramics》 2015年第3期31-43,共13页
Based on Maxwell’s constraint counting theory, rigidity percolation in GexSe1-x glasses occurs when the mean coordination number reaches the value of 2.4. This corresponds to Ge0.20Se0.80 glass. At this composition, ... Based on Maxwell’s constraint counting theory, rigidity percolation in GexSe1-x glasses occurs when the mean coordination number reaches the value of 2.4. This corresponds to Ge0.20Se0.80 glass. At this composition, the number of constraints experienced by an atom equals the number of degrees of freedom in three dimensions. Hence, at this composition, the network changes from a floppy phase to a rigid phase, and rigidity starts to percolate. In this work, we use reverse Monte Carlo (RMC) modeling to model the structure of Ge0.20Se0.80 glass by simulating its experimental total atomic pair distribution function (PDF) obtained via high energy synchrotron radiation. A three-dimensional configuration of 2836 atoms was obtained, from which we extracted the partial atomic pair distribution functions associated with Ge-Ge, Ge-Se and Se-Se real space correlations that are hard to extract experimentally from total scattering methods. Bond angle distributions, coordination numbers, mean coordination numbers and the number of floppy modes were also extracted and discussed. More structural insights about network topology at this composition were illustrated. The results indicate that in Ge0.20Se0.80 glass, Ge atoms break up and cross-link the Se chain structure, and form structural units that are four-fold coordinated (the GeSe4 tetrahedra). These tetrahedra form the basic building block and are connected via shared Se atoms or short Se chains. The extent of the intermediate ranged oscillations in real space (as extracted from the width of the first sharp diffraction peak) was found to be around 19.6 ?. The bonding schemes in this glass are consistent with the so-called “8-N” rule and can be interpreted in terms of a chemically ordered network model. 展开更多
关键词 Chalcogenide GLASSES rigidity PERCOLATION Reverse Monte Carlo modeling Atomic Pair Distribution Function (PDF) GexSe1-x GLASSES
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群伞减速系统刚柔耦合动力学建模与分析 被引量:1
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作者 王海涛 雷江利 荣伟 《航空学报》 北大核心 2025年第1期99-113,共15页
群伞减速系统被新一代可重复使用载人飞船普遍采用,对群伞系统进行动力学分析评估是航天器减速任务设计分析的重要环节。针对航天器群伞减速系统建立了多阶段、变结构、多维度刚柔耦合非线性多体动力学模型,分析了系统动力学模型的特点... 群伞减速系统被新一代可重复使用载人飞船普遍采用,对群伞系统进行动力学分析评估是航天器减速任务设计分析的重要环节。针对航天器群伞减速系统建立了多阶段、变结构、多维度刚柔耦合非线性多体动力学模型,分析了系统动力学模型的特点,指出群伞减速系统动力学具有复杂系统动力学的属性。通过仿真分析了航天器、减速伞和主伞在系统仿真中的动力学和运动参数,并对蒙特卡洛偏差仿真的结果进行了总结。仿真验证和分析结果表明,建立的刚柔耦合动力学模型能够准确模拟群伞减速系统工作过程和群伞碰撞等动力学行为。最后,针对降落伞减速系统动力学存在的问题和未来发展进行了分析和建议。 展开更多
关键词 群伞系统 刚柔耦合 复杂系统 动力学建模 减速
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冲击载荷下四足无人作战平台射击振动特性
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作者 刘坤 冯颖 +3 位作者 康宝 吴志林 宋杰 朱韬 《兵工学报》 北大核心 2025年第10期322-333,共12页
四足无人作战平台凭借其卓越的机动性和复杂地形适应能力,在未来战争中具有重大的军事应用价值。为探究冲击载荷对四足无人作战平台振动特性和射击精度的影响,建立了无人作战平台刚柔耦合发射动力学模型,通过数值仿真分析了不同冲击载... 四足无人作战平台凭借其卓越的机动性和复杂地形适应能力,在未来战争中具有重大的军事应用价值。为探究冲击载荷对四足无人作战平台振动特性和射击精度的影响,建立了无人作战平台刚柔耦合发射动力学模型,通过数值仿真分析了不同冲击载荷下枪口中心点绕x轴和z轴振幅、角位移及角速度变化规律,结合六自由度外弹道模型评估了射击散布特性,开展了有/无双向缓冲装置的无人作战平台实弹射击实验。结果表明:安装双向缓冲装置后,5连发射击时枪口中心点绕x轴和z轴方向振幅显著减小,振动量降低,角速度趋于稳定,未出现固定连接工况中持续增大现象,弹着点全数散布圆半径R 100减至86.4 mm,降幅34.6%。实弹测试数据显示,单发和5连发R 100分别为75.7 mm、94.5 mm,降低21.1%、32.8%,实验数据与仿真结果一致性较好,验证了数值仿真的准确性,证实了所设计的缓冲装置能有效抑制射击振动,大幅提高四足无人作战平台射击稳定性和精度,研究成果为无人作战平台结构优化设计提供了技术支撑。 展开更多
关键词 四足无人作战平台 振动特性 射击精度 刚柔耦合 动力学模型
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基于机构运动学奇异的多稳态特性设计与分析
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作者 李保坤 赵伟 李琳 《佳木斯大学学报(自然科学版)》 2025年第4期70-75,150,共7页
针对现有多稳态机构无法同时满足大位移行程和高精度的问题,设计出一种新型多稳态机构,建立机构的理论模型,根据虚功原理推导出两个串联双滑块四杆机构的运动静力学方程,得到滑块位移与驱动力和势能之间的关系。基于伪刚体模型法,用平... 针对现有多稳态机构无法同时满足大位移行程和高精度的问题,设计出一种新型多稳态机构,建立机构的理论模型,根据虚功原理推导出两个串联双滑块四杆机构的运动静力学方程,得到滑块位移与驱动力和势能之间的关系。基于伪刚体模型法,用平行四边形柔顺机构代替弹簧。对机构进行静力学仿真,研究不同的薄壁梁宽度和上滑块间的距离对机构稳态数目的影响。研究表明当薄壁梁宽度一定时,一定范围内缩短构件之间的距离,机构的稳态数目将会逐渐增加,最多出现6个稳态位置。当构件之间距离不变时,薄壁梁宽度每增加0.1mm,机构所需驱动力都要增大60%左右,机构整体势能增加80%左右。 展开更多
关键词 多稳态机构 虚功原理 运动静力学 伪刚体模型
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卫星单轴太阳翼驱动系统建模与控制技术综述
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作者 李朋 许瑞栋 +2 位作者 张家腾 高智刚 周军 《太阳能学报》 北大核心 2025年第6期142-151,共10页
针对目前卫星单轴太阳翼驱动系统面临的复杂问题,从系统建模、控制方法及地面验证等多角度全面梳理国内外的技术进展。首先分析太阳翼驱动系统的结构、原理和工作模式;进而针对其负载特性分别总结刚性和柔性太阳翼的动力学建模方法,并... 针对目前卫星单轴太阳翼驱动系统面临的复杂问题,从系统建模、控制方法及地面验证等多角度全面梳理国内外的技术进展。首先分析太阳翼驱动系统的结构、原理和工作模式;进而针对其负载特性分别总结刚性和柔性太阳翼的动力学建模方法,并针对非线性所带来的转速和角度控制难点探讨单一控制和复合控制策略,对各类算法作对比分析;然后介绍为提高地面试验验证的准确性所采用的微重力模拟和负载特性模拟方法。对未来航天器太阳翼驱动系统的研究动向进行总结与展望。 展开更多
关键词 太阳翼驱动系统 刚性负载 柔性负载 非线性建模 复合控制 地面验证
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双吸离心式水泵水轮机发电工况低水头不稳定内流特性研究
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作者 王超越 张宇雷 +3 位作者 陶然 潘家乐 李增怀 吴泽舟 《水电与抽水蓄能》 2025年第3期114-120,共7页
双吸离心式水泵水轮机在未来微型抽水蓄能中具有良好的应用前景。在低水头/小流量段,其单位转速-单位流量曲线上往往存在低水头不稳定工作区,极易导致机组在不同运行模式间跳动,严重影响安全稳定运行。相比于大型抽水蓄能常用的单吸式... 双吸离心式水泵水轮机在未来微型抽水蓄能中具有良好的应用前景。在低水头/小流量段,其单位转速-单位流量曲线上往往存在低水头不稳定工作区,极易导致机组在不同运行模式间跳动,严重影响安全稳定运行。相比于大型抽水蓄能常用的单吸式水泵水轮机,双吸式机组具有交错型双吸转轮及半螺旋形尾水管等特殊过流结构,故低水头不稳定流动必然有其独特性,但目前对于这种新型机组尚缺乏深刻认知。针对这一不足,本文基于自适应时间尺度驱动混合URANS/LES湍流模型及涡量二元分解理论,探究了双吸离心式水泵水轮机发电工况低水头不稳定内流特性,主要成果如下:①追踪了交错型双吸转轮做功能力随水头降低的劣化过程,量化了主要过流部件间能量分配比例的递变特征;②掌握了不同过流部件中主导涡结构的表观形式及涡旋强度分布特征,建立了总涡量与湍流耗散率间的非线性标度关系。研究成果有助于认识双吸离心式水泵水轮机低水头内流失稳过程,从而为这种新型机组的水力稳定性评估及调控提供科学依据。 展开更多
关键词 双吸离心式水泵水轮机 低水头工况 内流失稳 ATSD湍流模型 刚性涡量
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岩爆刚度理论研究进展与趋势展望
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作者 万荣基 肖亚勋 +2 位作者 丰光亮 赵同彬 尹延春 《金属矿山》 北大核心 2025年第9期207-216,共10页
岩爆是世界岩石力学与工程研究的前沿,也是制约我国深部战略实施的安全难题。岩爆防控的重点在于机理研究,而刚度理论是岩爆机理研究的重要内容。通过调研大量岩爆刚度理论研究文献,系统归纳了岩爆刚度理论的发展历程、试验方法与典型... 岩爆是世界岩石力学与工程研究的前沿,也是制约我国深部战略实施的安全难题。岩爆防控的重点在于机理研究,而刚度理论是岩爆机理研究的重要内容。通过调研大量岩爆刚度理论研究文献,系统归纳了岩爆刚度理论的发展历程、试验方法与典型试验结果、爆体—围岩系统模型与岩爆判据。研究表明:①刚度理论源于能量理论,经过丰富发展但仍难单一圆满解释岩爆机理;②刚度试验机演变推动了刚度理论试验由控制岩样刚度向控制试验机刚度转变,岩爆发生的必要条件是试验机刚度低于岩样,且其烈度随着两者刚度差增大而增大;③岩爆刚度系统模型将爆体与围岩视为弹塑性组合体,考虑岩样自身储能能力的系统模型更符合实际;④现有刚度计算方法主要围绕室内岩样和试验机,且基于刚度理论的岩爆判据仍局限于判别岩爆是否发生。通过分析刚度理论研究现有问题,展望了动态变刚度试验、不同等级岩爆的刚度理论判据与基于工程实例的原位岩爆刚度理论研究等进一步研究方向。分析结果可为岩爆刚度理论研究与工程应用提供参考。 展开更多
关键词 岩爆 刚度理论 刚性试验 系统模型 判据
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MODELING COMPLIANT NON-PENETRATION CONSTRAINT FOR VP MOTION SIMULATION 被引量:2
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作者 WangZheng TanJianrong LiuZhenyu JiYangjian 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2005年第2期163-168,共6页
A unilateral non-penetration constraint dynamical simulation model withfriction is constructed based on compliant model for mechanical system VP (virtual prototyping)simulation. This model combines computer graphics w... A unilateral non-penetration constraint dynamical simulation model withfriction is constructed based on compliant model for mechanical system VP (virtual prototyping)simulation. This model combines computer graphics with multi-body system dynamics. It avoidshandling multiplicity of solution, such as cases of no solution, multi-solution brought about byfriction during traditional construction of non-penetration constraint based on rigid model. At thesame time, the realism of VE (virtual environment) is improved in process of simulation.Furthermore, the valid condition of rolling and sliding unilateral contact is constituted based onsingular perturbation and linear complementary theory. Finally, the compliant method is verified byan interaction between a multi-legged robot and VE. 展开更多
关键词 Non-penetration constraint Compliant model rigid model DYNAMICS
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车体振动对刚性接触网-受电弓系统受流性能的影响 被引量:1
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作者 张程政 祁文延 +4 位作者 陈珍宝 巩译泽 张巍 陈阳 梅桂明 《电力机车与城轨车辆》 2025年第2期69-75,共7页
在城市轨道交通弓网系统关键动力学问题的研究中,车体振动及线路条件对弓网系统受流性能有重要影响。为此,文章基于有限元理论建立刚性接触网有限元模型,基于多体动力学理论和有限元仿真技术建立受电弓、车辆-轨道系统多刚体模型,并在... 在城市轨道交通弓网系统关键动力学问题的研究中,车体振动及线路条件对弓网系统受流性能有重要影响。为此,文章基于有限元理论建立刚性接触网有限元模型,基于多体动力学理论和有限元仿真技术建立受电弓、车辆-轨道系统多刚体模型,并在此基础上搭建完整的车-弓-网耦合动力学模型,研究车体振动对不同运行速度下刚性接触网-受电弓系统受流性能的影响,并对不同线路状态下车-弓-网系统受流性能进行研究分析。结果表明:在刚性接触网条件下,当列车运行速度较低时,由轨道激励引起的车体振动对弓网系统动力学性能产生一定的影响;而当列车运行速度较高时,车体振动对弓网系统动力学性能的影响更加明显,在仿真计算中不可忽略。线路条件对弓网系统受流质量的影响显著,尤其是列车运行速度较低时,恶劣的线路条件对弓网系统动力学性能的影响更为明显。 展开更多
关键词 车-弓-网耦合动力学模型 刚性接触网 车体振动 线路条件 受流性能
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基于前馈模型预测控制的阵风减缓技术研究
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作者 刘岳锋 段卓毅 +2 位作者 武虎子 齐万涛 刘桓宇 《飞行力学》 北大核心 2025年第2期36-41,共6页
采用激光雷达探测飞机前方阵风速度,并以此作为前馈信号设计综合前馈阵风信号和反馈过载信号的模型预测控制阵风减缓系统,能够充分利用激光雷达测量的阵风速度信号,使控制系统在阵风作用飞机前给出最优控制指令,从而提高阵风减缓性能。... 采用激光雷达探测飞机前方阵风速度,并以此作为前馈信号设计综合前馈阵风信号和反馈过载信号的模型预测控制阵风减缓系统,能够充分利用激光雷达测量的阵风速度信号,使控制系统在阵风作用飞机前给出最优控制指令,从而提高阵风减缓性能。建立了刚弹耦合的飞机阵风响应动力学模型,设计基于激光雷达和模型预测控制算法的阵风减缓控制系统,并以某型民用飞机为对象开展仿真研究。结果表明,利用激光雷达探测的阵风速度作为模型预测控制的前馈信号能够提高阵风减缓效果,且探测距离越远,阵风减缓率越高,但减缓率增加幅度会下降。 展开更多
关键词 激光雷达 阵风减缓 刚弹耦合 模型预测控制
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节段预制波形钢腹板组合箱梁桥节段 存放及吊装方案的优化设计 被引量:2
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作者 邓文琴 宋启港 +2 位作者 刘朵 彭宗卿 张建东 《江苏大学学报(自然科学版)》 CAS 北大核心 2025年第1期113-119,共7页
为了优化节段预制波形钢腹板组合箱梁桥节段划分、存放及吊装方案,以南京长江五桥引桥——立新路跨线桥为研究背景,采用数值模拟方法对波形钢腹板组合箱梁桥节段进行合理划分长度,分析标准节段梁存放及吊装期的应力变化及变形特征,并提... 为了优化节段预制波形钢腹板组合箱梁桥节段划分、存放及吊装方案,以南京长江五桥引桥——立新路跨线桥为研究背景,采用数值模拟方法对波形钢腹板组合箱梁桥节段进行合理划分长度,分析标准节段梁存放及吊装期的应力变化及变形特征,并提出合理的控制措施.结果表明:节段长度为240~400 cm时,对梁体抗弯承载力影响较小,波形钢腹板组合箱梁桥节段长度的合理划分取决于吊装及运输条件;节段梁存放层数不宜超过2层,如采用双层存放,需在波形钢腹板节段梁混凝土顶板与底板之间设置临时刚性支撑;节段梁吊装宜采用四吊点方案,即在靠近腹板处设置4个吊点,且起吊时在顶板与底板之间设置临时刚性支撑,以避免顶板变形过大,增加现场拼装控制的难度. 展开更多
关键词 波形钢腹板 节段预制 节段长度 存放阶段 吊装阶段 临时刚性支撑 有限元模型
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