期刊文献+
共找到182篇文章
< 1 2 10 >
每页显示 20 50 100
Experimental observation of fine secular frequency resonance oscillation with a rectilinear ion trap mass spectrometer
1
作者 Lixin Shan Zuojian Zhang +4 位作者 Zhiyang Wei Yongze Gao Zhiyuan Luo Shiyu Cheng Jinian Shu 《Chinese Journal of Chemical Physics》 CSCD 2024年第6期792-796,I0042,共6页
The mass resolution of the ordinary ion trap mass spectrometer derived from the quadrupole mass spectrometer usually ranges from hundreds to thousands.In this study,the fine secular frequency resonance oscillation was... The mass resolution of the ordinary ion trap mass spectrometer derived from the quadrupole mass spectrometer usually ranges from hundreds to thousands.In this study,the fine secular frequency resonance oscillation was observed with a rectilinear ion trap mass spectrometer.The FWHM of the responding resonance secular frequency of benzene was 0.012 kHz.The corresponding mass resolution was 8600 m/Δm for benzene(m/z=78).The mass spectrometer with secular frequency scanning has a linear response to benzene in the concentration range from 200 ppbv to 10000 ppbv.This study shows a new feature of the secular frequency scanning for ion trap mass spectrometers. 展开更多
关键词 Fine secular frequency Resonance oscillation Mass resolution rectilinear ion trap mass spectrometer
在线阅读 下载PDF
Arbitrary Rectilinear Block Packing Based on Less Flexibility First Principles
2
作者 杨中 董社勤 +1 位作者 洪先龙 吴有亮 《Journal of Semiconductors》 EI CAS CSCD 北大核心 2004年第11期1416-1422,共7页
The definition and formula of flexibility of arbitrary rectilinear blocks are introduced and LFF principles are extended to handle arbitrary rectilinear blocks and blocks with relative constraints.The experimental res... The definition and formula of flexibility of arbitrary rectilinear blocks are introduced and LFF principles are extended to handle arbitrary rectilinear blocks and blocks with relative constraints.The experimental results demonstrate the efficiency and effectiveness of the proposed method. 展开更多
关键词 LFF principles rectilinear block packing deterministic placement algorithm
在线阅读 下载PDF
Parametric Study of Low Frequency Broadband Rectilinear-to-Rotary Vibrational Energy Harvesting 被引量:1
3
作者 Chen Jingfan Deng Wei +1 位作者 Wang Ya Inman Dan 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2018年第1期1-9,共9页
A parametric study of a high-power-density dual resonator for achieving low frequency broadband electromagnetic energy harvesting is reported.The dual resonator consists of a rectilinear oscillator(R_LO)performing mag... A parametric study of a high-power-density dual resonator for achieving low frequency broadband electromagnetic energy harvesting is reported.The dual resonator consists of a rectilinear oscillator(R_LO)performing magnetic levitation and a rotary oscillator(R_TO)performing electromagnetic coupling through a stator and a rotor.Both oscillators,coupled by magnetic forces generated by a set of arc permanent magnets,radially magnetized and centro-symmetrically fixed onto the R_LO and the rotor of the R_TO achieve the reciprocating-to-rotary motion conversion and frequency up-conversion.Specifically,the dual resonator is able to convert stochastic reciprocating motion into controllable rotation,provide intrinsic frequency up-conversion,use non-contact magnetic coupling to provide near loss-free energy transfer and be configured into specific applications to obtain and maintain high-energy orbits of multi-stable energy harvesting.While solely focusing on developing a dual resonator provides substantial benefits,its dynamic behavior is unclear,thus electromagnetic-dynamic governing equations are derived,and a curve fitting model of restoring torque of R_TO under different repulsive magnets configurations are developed to predict key characteristics and to improve performance of the electromechanical system.Power analysis is carried out for providing aquantitative guidance of customizing the harvester to achieve an optimal power density. 展开更多
关键词 CURVE FITTING model NON-CONTACT rectilinear-to-rotary motion transformation frequency UP-CONVERSION systematic modeling parametric study
在线阅读 下载PDF
SHEAR EFFECTS ON LARGE AMPLITUDE FORCED VIBRATIONOF SYMMETRICALLY LAMINATED RECTILINEARLYORTHOTROPIC CIRCULAR PLATES
4
作者 徐加初 刘人怀 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 1998年第2期111-119,共9页
In this paper, nonlinear forced vibration of symmetrically laminated rectilinearly orthotropic circular plates excited by a harmonic force q(0)cos omega t including effects of transverse shear deformation is discussed... In this paper, nonlinear forced vibration of symmetrically laminated rectilinearly orthotropic circular plates excited by a harmonic force q(0)cos omega t including effects of transverse shear deformation is discussed. The analytical solution for the relationship between forcing frequency and amplitude of vibration is obtained by Galerkin's method. Finally, the paper analyses the effect of the transverse shear on the vibration of the plate and gives the ratio of nonlinear period to linear period for nonlinear free vibration of the plate. 展开更多
关键词 large amplitude forced vibration rectilinear orthotropy laminated circular plate transverse shear
在线阅读 下载PDF
地月空间编目系统观测体制研究
5
作者 陈艳玲 黄勇 王鹏 《中国图象图形学报》 北大核心 2025年第9期2966-2974,共9页
目的 地月空间非合作目标因缺乏合作信号的高精度测量手段,同时深空探测地面测控资源有限,以及在地月空间多体摄动环境条件下运动轨迹复杂需考虑完备的动力学模型,其编目定轨精度与时效性受到一定的制约和独特的挑战。方法 本文聚焦地... 目的 地月空间非合作目标因缺乏合作信号的高精度测量手段,同时深空探测地面测控资源有限,以及在地月空间多体摄动环境条件下运动轨迹复杂需考虑完备的动力学模型,其编目定轨精度与时效性受到一定的制约和独特的挑战。方法 本文聚焦地月空间非合作目标的编目定轨,提出基于天基光学观测技术的三体轨道约束条件下的空间目标编目定轨关键算法,以远距逆行轨道(distant retrograde orbit,DRO)和近直线晕轨道(near rectilinear halo orbit,NRHO)组成的地月空间卫星星座,模拟天基平台与空间目标的光学观测数据,利用仿真数据,采取动力学统计定轨算法,探讨了不同平台轨道误差、不同平台数量和平台分布,以及不同观测数据条件下的DRO、NRHO目标的编目定轨精度。结果 在天基平台轨道误差1 km、光学成像观测2″测量噪声水平、光压10%模型误差的仿真条件下,2DRO与2NRHO地月空间导航星座对DRO目标单站定轨精度为1~7 km,双站3天内每天观测3 h,定轨精度约1 km,预报1天轨道精度优于1.3 km;对于NRHO目标,单站观测3天定轨精度为1~3 km,双站每天观测3 h、6 h以及连续协同观测定轨精度分别优于1.2 km、1.1 km和1.0 km,这3种观测条件下预报1天轨道均方根误差(root mean square error, RMSE)分别优于3.0 km、2.5 km和1.9 km。结果表明,在天基测站误差1 km和3天定轨弧长的条件下,双站观测精度较单站观测有显著提高,双站每天观测3 h,针对DRO和NRHO目标的定轨精度均优于1.2 km,DRO轨道预报1天的精度优于1.3 km,NRHO轨道预报1天在连续观测3天的条件下精度最高,优于1.9 km。结论 本文采用完备的三体动力学模型,通过对典型地月空间目标光学定轨的多种场景仿真,发现双站每天3 h观测的编目定轨能力优于单站每天连续观测的定轨精度。这一结论对地月空间编目定轨观测效率和观测体制的规划和布局,以及地月空间区域的态势感知能力论证和分析有重要的工程应用价值。 展开更多
关键词 地月空间 非合作目标 天基光学观测 编目定轨 远距离逆行轨道(DRO) 近直线罩轨道(NRHO)
原文传递
基于NRHO的月球全球定位系统星座研究
6
作者 晋守聪 程潏 +1 位作者 刘磊 陈钢 《空间科学学报》 北大核心 2025年第2期317-327,共11页
针对未来月球探测与开发等任务对月球全球定位服务的需求,利用近直线晕轨道(NRHO)特殊的轨道空间几何特性,提出了以地月系NRHO作为参考轨道的月球全球定位系统(LGPS).首先,考虑轨道分布、卫星数目、轨道尺寸等星座构型参数,设计了多个... 针对未来月球探测与开发等任务对月球全球定位服务的需求,利用近直线晕轨道(NRHO)特殊的轨道空间几何特性,提出了以地月系NRHO作为参考轨道的月球全球定位系统(LGPS).首先,考虑轨道分布、卫星数目、轨道尺寸等星座构型参数,设计了多个星座构型方案;然后,从可见星数目、月球全球覆盖特性以及几何精度因子(GDOP)等方面,分析了不同构型参数对LGPS星座导航性能的影响.仿真结果表明,与Halo轨道相比,基于NRHO的LGPS在月球高纬度区域,尤其是对月球极区,具有更优的持续覆盖能力和定位精度,GDOP可达3以内.本文研究可对未来的月球开发任务提供导航定位方面的技术参考. 展开更多
关键词 月球全球定位系统 NRHO 导航星座 持续覆盖 定位精度
在线阅读 下载PDF
ACO-Steiner: Ant Colony Optimization Based Rectilinear Steiner Minimal Tree Algorithm 被引量:5
7
作者 胡昱 经彤 +3 位作者 冯哲 洪先龙 胡晓东 严桂英 《Journal of Computer Science & Technology》 SCIE EI CSCD 2006年第1期147-152,共6页
The rectilinear Steiner minimal tree (RSMT) problem is one of the fundamental problems in physical design, especially in routing, which is known to be NP-complete. This paper presents an algorithm, called ACO-Steine... The rectilinear Steiner minimal tree (RSMT) problem is one of the fundamental problems in physical design, especially in routing, which is known to be NP-complete. This paper presents an algorithm, called ACO-Steiner, for RSMT construction based on ant colony optimization (ACO). An RSMT is constructed with ants' movements in Hanan grid, and then the constraint of Hanan grid is broken to accelerate ants' movements to improve the performance of the algorithm. This algorithm has been implemented on a Sun workstation with Unix operating system and the results have been compared with the fastest exact RSMT algorithm, GeoSteiner 3.1 and a recent heuristic using batched greedy triple construction (BGTC). Experimental results show that ACO-Steiner can get a short running time and keep the high performance. Furthermore, it is Mso found that the ACO-Steiner can be easily extended to be used to some other problems, such as rectilinear Steiner minimal tree avoiding obstacles, and congestion reduction in global routing. 展开更多
关键词 rectilinear Steiner minimal tree (RSMT) ROUTING physical design ant colony optimization (ACO)
原文传递
Steiner Minimal Trees in Rectilinear and Octilinear Planes 被引量:1
8
作者 Song Pu SHANG Tong JING 《Acta Mathematica Sinica,English Series》 SCIE CSCD 2007年第9期1577-1586,共10页
This paper considers the Steiner Minimal Tree (SMT) problem in the rectilinear and octilinear planes. The study is motivated by the physical design of VLSI: The rectilinear case corresponds to the currently used M-... This paper considers the Steiner Minimal Tree (SMT) problem in the rectilinear and octilinear planes. The study is motivated by the physical design of VLSI: The rectilinear case corresponds to the currently used M-architecture, which uses either horizontal or vertical routing, while the octilinear case corresponds to a new routing technique, X-architecture, that is based on the pervasive use of diagonal directions. The experimental studies show that the X-architecture demonstrates a length reduction of more than 10-20%. In this paper, we make a theoretical study on the lengths of SMTs in these two planes. Our mathematical analysis confirms that the length reduction is significant as the previous experimental studies claimed, but the reduction for three points is not as significant as for two points. We also obtain the lower and upper bounds on the expected lengths of SMTs in these two planes for arbitrary number of points. 展开更多
关键词 Steiner minimal tree minimum spanning tree rectilinear plane octilinear plane
原文传递
Optimal circle-to-rectilinear orbit transfer with circumferential thrust 被引量:2
9
作者 Alessandro A.Quarta Giovanni Mengali Andrea Caruso 《Astrodynamics》 CSCD 2019年第1期31-43,共13页
This paper investigates the optimal transfer trajectories from a circular parking orbit towards the apocenter of a rectilinear ellipse,where the spacecraft reaches a quasi-stationary condition relative to an inertial ... This paper investigates the optimal transfer trajectories from a circular parking orbit towards the apocenter of a rectilinear ellipse,where the spacecraft reaches a quasi-stationary condition relative to an inertial reference frame.The spacecraft is equipped with a propulsion system that provides a circumferential continuous propulsive acceleration,that is,an acceleration whose direction is perpendicular to the primary body-spacecraft line.The performance index to minimize is the total flight time,and an indirect method is used to analyze the transfer trajectories.In this context,the optimal transfer performance is obtained as a function of the spacecraft propulsive acceleration magnitude through an interpolation procedure of numerical simulations.The results obtained with a continuous thrust propulsion system are also compared with those derived from a multi-impulse transfer.Finally,the paper investigates a heliocentric mission scenario in which the spacecraft minimizes the flight time required to reach a rectilinear ellipse with a given value of the aphelion radius. 展开更多
关键词 circumferential acceleration rectilinear ellipse optimal transfer preliminary mission analysis quasi-stationary condition
原文传递
近月空间三维周期轨道变轨策略研究
10
作者 屈琮渊 陈丹鹤 +2 位作者 刘培彦 罗敬升 Haddouche Abderrahman 《载人航天》 北大核心 2025年第5期578-586,共9页
近直线晕轨道(NRHO)与Butterfly轨道因其轨道立体特性,具有无月球遮挡通讯以及探测月球极区便利等优势,优先被考虑作为未来中继通信、载人登月等空间任务的中转轨道。出于卫星变轨任务需求,需要研究综合引力作用下地月空间中针对上述轨... 近直线晕轨道(NRHO)与Butterfly轨道因其轨道立体特性,具有无月球遮挡通讯以及探测月球极区便利等优势,优先被考虑作为未来中继通信、载人登月等空间任务的中转轨道。出于卫星变轨任务需求,需要研究综合引力作用下地月空间中针对上述轨道的低能量变轨方案。基于双圆限制性四体系统,设计了针对NRHO和Butterfly轨道的双脉冲方案。首先基于微分修正方法计算了目标转移轨道族,其次计算了双圆四体系统下由周期共振比2∶1月球周期的L2南NRHO至不同周期NRHO和Butterfly轨道的最优变轨相位族。仿真表明,变轨相位与脉冲消耗不随目标轨道变化呈现单调增减性质,最优转移轨道由多个解集拼接而成,且四体系统最优变轨脉冲消耗与转移时间小于三体系统。针对南族NRHO内转移,脉冲消耗范围为(0.007 km/s,0.096 km/s),至北族NRHO转移消耗范围是(0.079 km/s,0.195 km/s),至But-terfly轨道脉冲消耗范围是(0.121 km/s,0.169 km/s)。 展开更多
关键词 双圆四体模型 NRHO Butterfly轨道 变轨策略 轨道优化
在线阅读 下载PDF
A Kind of Rectilinear Congruences in the Minkowski 3-Space
11
作者 侯中华 李丽 《Journal of Mathematical Research and Exposition》 CSCD 北大核心 2008年第4期911-918,共8页
We consider the rectilinear congruence T generated by the tangents to a one parameter family of geodesics on a space-like surface S1 in the Minkowski 3-space E13, having S1 as one of its focal surfaces. We prove that ... We consider the rectilinear congruence T generated by the tangents to a one parameter family of geodesics on a space-like surface S1 in the Minkowski 3-space E13, having S1 as one of its focal surfaces. We prove that the two families of torsal surfaces of T touch the second focal surface S2 along the net of orthogonal parametric curves if and only if S1 is developable. We also obtain the necessary and sufficient condition for the correspondence between the points of S1 and S2 at the same rays preserving the... 展开更多
关键词 the rectilinear congruence the focal surfaces the Minkowski space the space-like surface maximal surfaces.
在线阅读 下载PDF
GENERAL THEORETICAL RESULTS ON RECTILINEAR EMBEDABILITY OF GRAPHS
12
作者 刘彦佩 A.MORGANA B.SIMEONE 《Acta Mathematicae Applicatae Sinica》 SCIE CSCD 1991年第2期187-192,共6页
In the design of certain kinds of electronic circuits the following question arises:given a non-negative integer k, what graphs admit of a plane embedding such that every edge is a broken lineformed by horizontal and ... In the design of certain kinds of electronic circuits the following question arises:given a non-negative integer k, what graphs admit of a plane embedding such that every edge is a broken lineformed by horizontal and vertical segments and having at mort k bends? Any such graph is said tobe k--rectilinear. No matter what k is, an obvious necessary condition for k-rectilinearity is that thedegree of each vertex does not exceed four.Our main result is that every planar graph H satisfying this condition is 3--rectilinear:in fact,it is 2--rectilinear with the only exception of the octahedron. We also outline a polynomial-timealgorithm which actually constructs a plane embedding of H with at most 2 bends (3 bends if H isthe octahedron) on each edge. The resulting embedding has the property that the total number ofbends does not exceed 2n, where n is the number of vertices of H. 展开更多
关键词 LINE GENERAL THEORETICAL RESULTS ON rectilinear EMBEDABILITY OF GRAPHS
原文传递
长期拟周期近直线晕轨道高效设计方法 被引量:2
13
作者 秦理民 杨洪伟 李爽 《宇航学报》 EI CAS CSCD 北大核心 2024年第1期43-51,共9页
面向未来近月空间站部署需求,提出了一种三级修正的长期拟周期近直线晕轨道(NRHO)设计方法。首先,设计了新的离散点选取策略,降低了对参数敏感区域的打靶需求,提高了多点打靶法计算多圈次拟周期NRHO的收敛性能。然后,基于NRHO的对称特性... 面向未来近月空间站部署需求,提出了一种三级修正的长期拟周期近直线晕轨道(NRHO)设计方法。首先,设计了新的离散点选取策略,降低了对参数敏感区域的打靶需求,提高了多点打靶法计算多圈次拟周期NRHO的收敛性能。然后,基于NRHO的对称特性,给出了初始拟周期NRHO圈次延续方法和滚动时域长期拟周期NRHO生成方法,根据拟周期NRHO近月点半径设计了修正策略。使用不同的NRHO进行仿真实验,生成了维持500圈约10年的长期拟周期NRHO。仿真结果表明本方法提高了收敛效率,且能有效生成地月空间长期拟周期NRHO。 展开更多
关键词 地月空间 拟周期近直线晕轨道 多点打靶法 轨道设计
在线阅读 下载PDF
基于三体问题的地月空间中转站轨道设计
14
作者 彭蕾 梁玉莹 +1 位作者 师鹏 景前锋 《飞行力学》 CSCD 北大核心 2024年第5期26-33,共8页
针对未来地月空间中转站的建设需求,进行中转站轨道选择与转移轨迹设计。基于地月空间周期轨道,综合考虑轨道构型、稳定性等因素,选定L_(2)点的南近直线晕轨道(NRHO)作为目标轨道。针对NRHO稳定性强、转移难以实现的问题,基于三体Lamber... 针对未来地月空间中转站的建设需求,进行中转站轨道选择与转移轨迹设计。基于地月空间周期轨道,综合考虑轨道构型、稳定性等因素,选定L_(2)点的南近直线晕轨道(NRHO)作为目标轨道。针对NRHO稳定性强、转移难以实现的问题,基于三体Lambert算法通过月球借力从奔月轨道转移到NRHO。为克服NRHO无明显流形结构的缺陷,基于Cauchy-Green张量提出相空间主拉伸方向理论,进而拼接Lambert段与沿主拉伸方向的反向积分轨迹,获得施加转移脉冲的最有效方向,求解低能转移轨迹。研究结果表明,月球借力转移可以用于载人探月,Lambert拼接法能有效缩短低能转移的时间,为中转站货运提供轨道参考。 展开更多
关键词 地月空间中转站 NRHO 主拉伸方向 三体Lambert算法
原文传递
SOME COMBINATORIAL OPTIMIZATION PROBLEMS ARISING FROM VLSI CIRCUIT DESIGN 被引量:2
15
作者 刘彦佩 《Applied Mathematics(A Journal of Chinese Universities)》 SCIE CSCD 1993年第2期218-235,共18页
This paper is basically a survey to show a number of combinatorial optimization problems arising from VLSI circuit design. Some of them including the existence problem, minimax problem, net representation, bend minimi... This paper is basically a survey to show a number of combinatorial optimization problems arising from VLSI circuit design. Some of them including the existence problem, minimax problem, net representation, bend minimization, area minimization, placement problem, routing problem, etc. are especially discussed with new results and theoretical ideas for treating them. Finally, a number of problems for further research are mentioned. 展开更多
关键词 VLSI Circuit Design rectilinear Embedding rectilinear Convexity Forbidden Configuration Combinatorial Optimization.
在线阅读 下载PDF
小型矩形离子阱质谱仪的研制 被引量:13
16
作者 姜杰 费强 +7 位作者 金伟 李明 庞晓东 李彬 范志勇 许晓宇 周建光 金钦汉 《分析化学》 SCIE EI CAS CSCD 北大核心 2007年第9期1387-1390,共4页
研制的小型质谱仪以电子轰击源(EI)和矩形离子阱(RIT)质量分析器为核心部件,采用渗透阀控制的直接进样系统,高增益的电子倍增器用于离子检测,通过小信号放大系统对电子倍增器输出的弱电流再次放大,并输出电压信号,计算机上的NI数据采集... 研制的小型质谱仪以电子轰击源(EI)和矩形离子阱(RIT)质量分析器为核心部件,采用渗透阀控制的直接进样系统,高增益的电子倍增器用于离子检测,通过小信号放大系统对电子倍增器输出的弱电流再次放大,并输出电压信号,计算机上的NI数据采集卡和Labview操作软件对电压信号进行采集处理。由旋片机械泵和分子泵组成的真空系统可以形成10-5Pa的质谱工作环境。对研制的仪器进行了初步测试,得到了相应的质谱图,通过质量校正表明,结果令人满意。 展开更多
关键词 矩形离子阱 质谱 电子轰击源
在线阅读 下载PDF
直线振动筛运动学参数的确定 被引量:31
17
作者 李玉凤 李永志 +2 位作者 潘东明 张学成 鲍玉新 《煤矿机械》 北大核心 2008年第3期33-34,共2页
通过分析直线振动筛的工作原理,阐述其运动学参数在不同工作状态下的确定原则,给出具体的计算公式,并给出实例进行了具体的参数计算,为今后直线振动筛的设计提供重要参考。
关键词 直线振动筛 工作原理 运动学参数
在线阅读 下载PDF
元胞自动机最短路径算法优化 被引量:10
18
作者 任志国 郭健 +2 位作者 李爱光 王卉 阚映红 《遥感学报》 EI CSCD 北大核心 2015年第1期108-115,共8页
概括了当前GIS中最短路径算法,分析了元胞自动机在最短路径分析算法中的原理及应用现状,并从两个方面对基于元胞自动机的最短路径算法进行优化即直线优化的元胞自动机最短路径算法。(1)将A*算法中的启发函数引入元胞自动机模型,提出了... 概括了当前GIS中最短路径算法,分析了元胞自动机在最短路径分析算法中的原理及应用现状,并从两个方面对基于元胞自动机的最短路径算法进行优化即直线优化的元胞自动机最短路径算法。(1)将A*算法中的启发函数引入元胞自动机模型,提出了直线优化元胞自动机最短路径模型;(2)考虑道路网特征对最短路径算法的影响,得出具有道路网自适应性的最短路径分析模型。最后选取不同形态特征的shp道路网数据,验证了优化算法在实际应用中的适用性和高效性。 展开更多
关键词 元胞自动机 A^*算法 直线优化 道路网特征 启发式搜索
原文传递
飞机起飞着陆性能仿真与分析 被引量:22
19
作者 林可心 岑国平 +1 位作者 李乐 刘钢 《空军工程大学学报(自然科学版)》 CSCD 北大核心 2012年第4期21-25,共5页
为真实反映飞机起飞着陆的滑跑过程,记录了某型飞机的速度、加速度传感器现场数据,建立了飞机起飞着陆滑跑过程的微分方程并进行了解算;基于飞机滑跑过程的微分方程采用Simulink对飞机起降性能进行建模和仿真,记录数据、理论结果和仿真... 为真实反映飞机起飞着陆的滑跑过程,记录了某型飞机的速度、加速度传感器现场数据,建立了飞机起飞着陆滑跑过程的微分方程并进行了解算;基于飞机滑跑过程的微分方程采用Simulink对飞机起降性能进行建模和仿真,记录数据、理论结果和仿真结果三者对比验证了所建立的仿真模型是有效的。基于该模型对该飞机滑跑过程进行仿真分析,结果表明起飞和不放阻力伞着陆过程可近似为匀加速直线运动过程,放阻力伞着陆过程则比较复杂。最后,研究3个主要参数对滑跑距离的影响,结果表明滑跑距离与机场海拔和风速呈近似线性关系,与迎角呈非线性关系且在迎角为8°时存在极小值点。 展开更多
关键词 飞机起降性能 微分方程 匀加速直线运动
在线阅读 下载PDF
非直角互连——布线技术发展的新趋势 被引量:8
20
作者 洪先龙 朱祺 +3 位作者 经彤 王垠 杨旸 蔡懿慈 《Journal of Semiconductors》 EI CAS CSCD 北大核心 2003年第3期225-233,共9页
由于集成电路制造工艺的不断提高 ,集成电路的设计规模遵循Moore定律持续向前发展 ,并出现了系统级芯片 (SOC)这一新的集成电路设计概念 .同时遇到的困难之一是互连线成为影响电路性能的决定因素 :芯片速度变慢、功耗增大、噪声干扰加... 由于集成电路制造工艺的不断提高 ,集成电路的设计规模遵循Moore定律持续向前发展 ,并出现了系统级芯片 (SOC)这一新的集成电路设计概念 .同时遇到的困难之一是互连线成为影响电路性能的决定因素 :芯片速度变慢、功耗增大、噪声干扰加剧 .若采用以往基于直角互连结构的基础模型进行互连线性能的优化 ,其能力受到限制 .于是 ,人们试图采用其他互连结构作为突破途径 ,以实现高性能的集成电路 .在这种技术需求与目前工艺支持的背景下 ,从 2 0世纪 90年代初出现的关于非直角互连的零散的、试探性的研究 ,将成为国际上布线领域新的热点研究方向 .文中将针对非直角布线方面以往零散的研究工作进行总结与分析 ,指出了目前需要解决的关键技术 ,并结合自己的研究工作基础提出了可行的技术路线与设想 . 展开更多
关键词 布线 λ-几何结构 非直角互连 系统级芯片 集成电路
在线阅读 下载PDF
上一页 1 2 10 下一页 到第
使用帮助 返回顶部