Plane Design(平面设计)研究综述
Plane Design 平面设计 - We prove that if $G$ is an almost simple group with socle a finite simple group of Lie type, then $\mathcal{D}$ is either the point-hyperplane design of a projective space $\mathrm{PG}_{n-1}(q)$, or it is of parameters $(7,4,2)$, $(11,5,2)$, $(11,6,2)$ or $(45,12,3)$. [1] Our approach opens the door to applying machine learning to large-scale physical modeling tasks like airplane design and climate prediction. [2] As the wiring space on the printed circuit board becomes more and more tight, especially in the high-speed backplane design, it is impossible for all high-speed signal lines to be laid on the top and bottom layers on the traditional coplanar waveguides. [3] The formal and rigorous certification process and training, coupled with the many technological advances in airplane design and equipment, have made commercial air flight safer today than ever. [4] Modern day VTOL fixed-wing aircraft based on quadplane design is relatively simple and reliable due to lack of complex mechanical components compared to tilt-wings or tilt-rotors in the pre-80’s era. [5] These include 1) the hydrostatic and hydrodynamic problems associated with seaplane design, 2) early-stage methods for sizing the hull, 3) prediction techniques using archival data, and 4) hydrodynamic model testing procedures. [6] The transition uses an in-plane design which enables low-loss integration of micromachined waveguide components, as it eliminates the need for waveguide bends and complex multi-layer structures. [7] The off-plane design of CIP structures endows MSEF excellent field-dependent deformability and actuation ability. [8] It shows that backplane designs with large Decision Feedback Equalizer (DFE) taps can have significant error propagation effect, which degrades the system performance further. [9] Bird strike analysis has been an essential work in aeroplane design and airworthiness assessment. [10] The current study investigates the application of statistical methods to flight, which have been used in science over time to understand complex physical and mathematical systems by using randomly generated numbers as input into those systems to generate a range of solutions and, specifically, how mathematics is used to examine airplane design and crash frequency. [11] Prediction of take-off performance, involving aerodynamic analysis and hydrodynamic analysis, is a main challenge in seaplane design, while the prediction methods have been little improved since the 1960s. [12] This paper deals with porosity-based topology optimization of forced convection planar heat sinks considering out-of-plane design-dependent deformation problems. [13] This paper describes a methodology to build a high bandwidth, scalable first approximation circuit model using simple transmission lines of long vias typically used in thick backplane designs. [14] Historically, the earliest concern on fluid–solid interaction (FSI) problems is with airplane design, and the related well-developed FSI theory is termed aeroelasticity, in which the air is considered a compressible fluid, and the main aim of analysis is to determine the critical speed of airplane flutter. [15] The use of autonomous fighters and bombers to destroy enemy targets is especially promising because of the lack of training required for robotic pilots, autonomous planes are capable of performing maneuvers which could not otherwise be done with human pilots (due to high amount of G-force), plane designs do not require a life support system, and a loss of a plane does not mean a loss of a pilot. [16] There is no a priori reason why this should not apply as well to human behaviour as it does to the theory of aerodynamics informing airplane design, for example. [17] Virtual testing and hybrid simulation have become an important trend in airplane design and validation. [18] The rationality of the proposed ESD damage model for interlayer Cu interconnection is verified, which provides a theoretical basis for subsequent IGZO TFT backplane design with high robustness. [19] The aeroelastic stability of airplanes is one of the most important aspects of airplane design. [20] Purpose The purpose of this paper is to attempt an aerospaceplane design with the objective of Low-Earth-Orbit-and-Return-to-Earth (LEOARTE) under the constraints of safety, low cost, reliability, low maintenance, aircraft-like operation and environmental compatibility. [21] This is the reason that all-electric aeroplane is the major aspect in research of aeroplane design. [22] The BWB300 is a 300-seat Blended Wing Body airplane designed by the Airplane Concept Design Institute of Northwestern Polytechnical University. [23] This study considers the optimization of a hybrid-electric aircraft for thin-haul operations and investigates how the airplane design can be modularized to enable a multi-design-point optimization. [24] Until now, the most common sailplane used in Indonesia is still Schweitzer SGS 1-26, which is a single seated metal-fabric sailplane designed in 1955 and produced until 1979. [25] The connection concept of placing only two bolts in offset misalignment against the bending load along the wing span was used for an aerobatic airplane designed in Thailand as a KIT plane to minimize the impact of drilling numerous holes. [26]我们证明如果 $G$ 是一个近乎单群且 socle 是一个李型有限单群，那么 $\mathcal{D}$ 要么是一个射影空间 $\mathrm{PG}_{n 的点超平面设计-1}(q)$，或者是参数$(7,4,2)$, $(11,5,2)$, $(11,6,2)$ or $(45,12,3) )$。 [1] 我们的方法为将机器学习应用于飞机设计和气候预测等大规模物理建模任务打开了大门。 [2] 随着印制电路板上的布线空间越来越紧，特别是在高速背板设计中，不可能在传统的共面波导上将所有高速信号线都铺设在顶层和底层。 [3] 正式和严格的认证过程和培训，加上飞机设计和设备方面的许多技术进步，使今天的商业航空飞行比以往任何时候都更加安全。 [4] 现代 基于四翼设计的垂直起降固定翼飞机由于缺乏复杂性，相对简单可靠 机械部件相比 80 年代前的倾斜翼或倾斜旋翼。 [5] 其中包括 1) 与水上飞机设计相关的流体静力和流体动力学问题，2) 船体尺寸确定的早期方法，3) 使用档案数据的预测技术，以及 4) 流体动力学模型测试程序。 [6] 该过渡采用平面内设计，可实现微加工波导组件的低损耗集成，因为它消除了对波导弯曲和复杂多层结构的需求。 [7] CIP 结构的平面外设计赋予 MSEF 优异的场相关变形能力和驱动能力。 [8] 它表明具有大决策反馈均衡器 (DFE) 抽头的背板设计会产生显着的错误传播效应，从而进一步降低系统性能。 [9] 鸟击分析一直是飞机设计和适航评估中的一项重要工作。 [10] 目前的研究调查了统计方法在飞行中的应用，随着时间的推移，这些方法已在科学中用于理解复杂的物理和数学系统，方法是使用随机生成的数字作为这些系统的输入来生成一系列解决方案，特别是数学是如何实现的用于检查飞机设计和碰撞频率。 [11] 起飞性能的预测，包括空气动力分析和水动力分析，是水上飞机设计的主要挑战，而预测方法自 1960 年代以来几乎没有改进。 [12] 本文讨论了考虑平面外设计相关变形问题的强制对流平面散热器基于孔隙率的拓扑优化。 [13] 本文介绍了一种使用通常用于厚背板设计的长通孔的简单传输线来构建高带宽、可扩展的第一近似电路模型的方法。 [14] 历史上，对流固耦合 (FSI) 问题的最早关注是飞机设计，而相关发达的 FSI 理论被称为气动弹性，其中空气被视为可压缩流体，分析的主要目的是确定飞机颤振的临界速度。 [15] 使用自主战斗机和轰炸机摧毁敌方目标尤其有希望，因为机器人飞行员缺乏所需的训练，自主飞机能够执行人类飞行员无法完成的机动（由于大量的 G 力)，飞机设计不需要生命支持系统，一架飞机的损失并不意味着飞行员的损失。 [16] 例如，没有先验的理由表明，它不应该适用于人类行为，因为它适用于为飞机设计提供信息的空气动力学理论。 [17] 虚拟测试和混合仿真已成为飞机设计和验证的重要趋势。 [18] 验证了所提出的层间Cu互连ESD损伤模型的合理性，为后续的高鲁棒性IGZO TFT背板设计提供了理论依据。 [19] 飞机的气动弹性稳定性是飞机设计中最重要的方面之一。 [20] 目的 本文的目的是在安全、低成本、可靠性、低维护、类似飞机操作和环境兼容性。 [21] 这就是全电动飞机成为飞机设计研究的主要方面的原因。 [22] BWB300是由西北工业大学飞机概念设计院设计的300座融合翼体飞机。 [23] 本研究考虑了混合动力电动飞机用于薄程运营的优化，并研究了如何将飞机设计模块化以实现多设计点优化。 [24] 直到现在，印度尼西亚最常用的滑翔机仍然是 Schweitzer SGS 1-26，这是一种单座金属织物滑翔机，设计于 1955 年，生产到 1979 年。 [25] 在泰国设计的一架特技飞机作为 KIT 飞机使用了仅放置两个螺栓以抵消沿翼展的弯曲载荷的连接概念，以最大程度地减少钻孔大量孔的影响。 [26]
Control Plane Design 控制平面设计
Results indicate that a time-sensitive network control plane design is feasible, and its pros and cons are discussed. [1] In the network planning of software-defined optical networks (SDONs), the control plane design is of great importance because it directly affects the performance and reliability of network control and management (NC&M). [2] Although reliable controller placement and control plane design was thoroughly investigated in SDNs, there was a lack of attention for resilient hypervisor placement and control path design for vSDNs. [3] The numerical results show that our proposed control plane design performs better than existing control plane designs where control traffic is statistically multiplexed with data traffic in terms of delay in the control plane and blocking probability in the data plane. [4] Further, we analyze the need of frequent control plane adaptation, and compare different control plane design choices according to a novel flexibility measure. [5] In this paper we present a high-speed control plane design based on a central switch scheduler for nanosecond optical switching which significantly reduces the end-to-end latency in the network compared to using the best electronic switches. [6] The design of the user equipment (UE) state machine is one of the central questions related to the overall control plane design. [7]结果表明时间敏感的网络控制平面设计是可行的，并讨论了其优缺点。 [1] 在软件定义光网络（SDON）的网络规划中，控制平面的设计非常重要，因为它直接影响到网络控制和管理（NC&M）的性能和可靠性。 [2] 尽管在 SDN 中对可靠的控制器布局和控制平面设计进行了深入研究，但对 vSDN 的弹性管理程序布局和控制路径设计缺乏关注。 [3] 数值结果表明，我们提出的控制平面设计在控制平面延迟和数据平面阻塞概率方面优于现有控制平面设计，其中控制流量与数据流量在统计上多路复用。 [4] 此外，我们分析了频繁调整控制平面的需求，并根据新的灵活性度量比较了不同的控制平面设计选择。 [5] 在本文中，我们提出了一种基于用于纳秒级光交换的中央交换机调度程序的高速控制平面设计，与使用最佳电子交换机相比，它显着降低了网络中的端到端延迟。 [6] 用户设备 (UE) 状态机的设计是与整体控制平面设计相关的核心问题之一。 [7]
Focal Plane Design
According to the results obtained we have optimized the focal plane design of the telescope. [1] A novel focal plane design is optimized to observe the UV air fluorescence signal from extensive air showers (EASs) in a stereoscopic UHECR observation mode and the Cherenkov signals from EASs from UHECRs and neutrino-induced τ-leptons in an Earth-limb viewing mode. [2]根据获得的结果，我们优化了望远镜的焦平面设计。 [1] 优化了一种新颖的焦平面设计，以在立体 UHECR 观察模式下观察来自广泛空气簇射 (EAS) 的紫外空气荧光信号，以及在地球肢体观察模式下观察来自 UHECR 和中微子诱导的 τ 轻子的 EAS 的切伦科夫信号。 [2]
Datum Plane Design
p4 with additional resources spared, offering itself as a compelling solution for switch data plane designers. [1] The data plane design comprises a flow counter table and a flow key table for storing flow-level data. [2]p4 节省了额外的资源，为交换机数据平面设计人员提供了引人注目的解决方案。 [1] 数据平面设计包括流计数器表和流键表，用于存储流级数据。 [2]