运输网络的最短有向路Petri网仿真算法

随着对综合交通体系和智能交通研究的逐步深入,发现必须解决运输需求和运输网络分析的技术问题。在已有的方法中,只有对有向网络有比较成熟的理论和方法,然而,运输网络却是无向的。本文内容是论述如何借助于Petri网论和Petri网图计算机仿真将无向交通运输网络转换为Petri网表示的有向图,并同时求出相应的运输网络中OD（起点终点）对的最短有向路径及路长。本文以图的形式给出Petri网的定义,通过导入“时间Place”和“标记”的附加描述,使Petri网成为扩充的Petri网（EPN）。定义Petri网图仿真器的运行规则和步骤,用Petri网图仿真器、自动将无向运输网络转换成EPN模型,然后自动求出相应的最短有向路径和路长。通过显示、打印或电信号,为用户提供信真报告或电信号。     

阿伦故事美女大揭密--访中国最大酒吧连锁

到了成都哪里都可以不去，但阿伦故事是不能不去的一个地方，网上流行的一句话：“如果男人喊你不要去阿伦故事一定是他对自己没有信心！女人喊你不要去阿伦故事，她一定是怕自己被抛弃！”     

阆中:古韵幽幽惬意人生

豕突狼奔的快节奏，终于在阆中古城戛然而止，我们开始感觉她的缓慢，感悟她的古朴，阅读她的历史，抚摩她的宁静。2300多年会遗忘很多，也会留下很多，留下的是传说，历史还有风水古城。华胥的踪迹只能在典籍中云寻找，人们偶尔会在岸边结网捕鱼，但他们并不会询问这是否源于伏羲！     

激光选区烧结金属粉末的研究

A series of experiments are carried out with selective laser sintering(SLS) for copper,copper-nickel powder matetials.The phenomena of the sintering process is ana-lyzed,the influence of techmological parameters is dis-cussed in detail,By means of SEM with energy spectrum system and X-ray diffraction spectrum,the morphology of the microstructure and the compositions of the different zones are analyzed,the mechanism of the laser sintering metallic powders is preliminarily explored,All those above lay the foundations for the forming metal parts by laser sintering metallic powders.     

直升机旋翼旋转状态下浆叶固有频率的测试

直升机旋翼固有频率的合理配置是其动力学设计的关键之一，除了分析计算外，在型号研制中还必须进行试验校验。本文介绍了一种对全尺寸旋翼在旋转状态下通过自动倾斜器激振，对应变响应的分析找出其固有频率的试验方法。针对旋翼试验中干扰因素多等特点，提出了一种将时域数据分段处理的新方法，在找挥舞二阶固有频率的过程中，经过认真的分析研究，对一个与之接近的频率给出了合理的解释。     

研究计划管理系统的Petri网论法

本文以图的形式给出Petri网的定义;通过导入“时间Place”和“象征”的附加描述,使Petri网成为扩充的Petri网(EPN);用EPN模拟计划管理系统,用EPN仿真器构画计划管理系统的图模型、求系统的时间参数、进行系统的优化。     

有限大平板中圆孔的应力集中计算

本文应用广义变分原理,给出了含圆孔的有限大平板应力集中的计算公式。並对矩形板单向均匀拉伸和剪切两种情况进行了数值计算,将计算结果绘成了曲线。     

柔性航天器姿态机动的时间次优反馈控制

研究了由一个中心刚体带若干柔性附件的航天器姿态反馈控制问题。利用相平面分析的方法给出了一种近似时间最优的反馈开关控制逻辑。仿真结果表明，些控制逻辑能够实现静止一静止的姿态机动，并且对附件振动有抑制作用。     

Performance improvement of real-time PPP ambiguity resolution using a regional integer clock

Obtaining reliable GNSS uncalibrated phase delay (UPD) or integer clock products is the key to achieving ambiguity-fixed solutions for real-time (RT) precise point positioning (PPP) users. However, due to the influence of RT orbit errors, the quality of UPD/integer clock products estimated with a globally distributed GNSS network is difficult to ensure, thereby affecting the ambiguity resolution (AR) performance of RT-PPP. In this contribution, by fully utilising the consistency of orbital errors in regional GNSS network coverage areas, a method is proposed for estimating regional integer clock products to compensate for RT orbit errors. Based on Centre National d’Études Spatiales (CNES) RT precise products, the regional GPS/BDS integer clock was estimated with a CORS network in the west of China. Results showed that the difference between the estimated regional and CNES global integer clock/bias products was generally less than 5 cm for GPS, whereas clock differences of greater than 10 cm were observed for BDS due to the large RT orbit error. Compared with PPP using global integer clock/bias products, the AR performance of PPP using the regional integer clock was obviously improved for four rover stations. For single GPS, the horizontal and vertical accuracies of ambiguity-fixed PPP solutions were improved by 56.2% and 45.3% on average, respectively, whereas improvements of 67.5% and 50.5% in the horizontal and vertical directions, respectively, were observed for the combined GPS/BDS situation. Based on a regional integer clock, the RMS error of a kinematic ambiguity-fixed PPP solution in the horizontal direction could reach 0.5 cm. In terms of initialisation time, the average time to first fix (TTFF) in combined GPS/BDS PPP was shortened from 18.2 min to 12.7 min. In view of the high AR performance realised with the use of regional integer clocks, this method can be applied to scenarios that require high positioning accuracy, such as deformation monitoring.     

Integrated guidance and control for solar sail station-keeping with optical degradation

Current control approaches for solar sail station-keeping on libration point orbits have not considered the degradation of the sail’s optical properties. However, significant optical degradation could lead to poor station-keeping performance or even complete failure. This paper presents an integrated guidance and control strategy to address this problem by updating the reference orbit based on in situ estimation. An exponential optical degradation model is incorporated into the solar radiation acceleration model, and an on-line reference orbit update approach is incorporated into the station-keeping, coupled with an active disturbance rejection controller. The reflection coefficient is estimated on-line and the reference orbit is updated discretely when the optical properties have degraded by a prescribed amount. This strategy provides discrete updates to the reference orbits such that the perturbation due to the optical degradation is maintained within a small range. These smaller perturbations can be dealt with by the controller’s robustness and station-keeping can be sustained for long durations even in the presence of large optical degradation.