高稳定度X射线脉冲星信号模拟

X射线脉冲星导航是一种完全自主的导航方式, 在深空乃至行星际空间具有潜在的工程应用价值.由于空间飞行试验系统复杂, 成本巨大, 在实验室环境下高精度地模拟X射线脉冲星信号对数据处理方法和导航方案的验证具有重要意义. 针对当前机械转盘式模拟系统中时间稳定度和轮廓精度的不足, 提出了一种通过产生的轮廓电压信号直接控制可见光光源, 再利用衰减获得光子流, 最后经单光子探测和处理电路输出光子到达时间序列的模拟新方法.该方法实现成本低, 支持任意X射线脉冲星信号的模拟, 且具有高时间稳定度和轮廓精度. 详细地讨论了该方法的原理和涉及的关键技术, 搭建了X射线脉冲星信号模拟系统, 并进行了实验. 实验结果表明: 该系统大幅提高了X射线脉冲星信号的模拟效果, 将模拟脉冲星自转周期的稳定度从现有的10^-4提高到10^-9; 当探测器面积为1 m², 探测能谱范围为2–10 keV, 积分时间为1200 s时, 模拟的PSR B1509-58 观测脉冲轮廓与标准脉冲轮廓的相关系数达到了0.993. 关键词： X 射线光子信号 时间稳定度 观测脉冲轮廓 导航算法     

Research on the estimation method of DVL velocity error based on double program in Fiber Optic Gyro SINS

As a basic velocity, DVL is introduced in the navigation solution process of Fiber Optic Gyro Strapdown Inertial Navigation System (FOG SINS). According to the special application background, DVL error is unavoidable to be introduced to navigation information that is calculated by FOG SINS. Firstly, the effect of DVL error on steady-state error of misalignment angles is derived. Secondly, the estimation method of DVL error is proposed: the DVL velocity error is calculated by attitude information, which is resolved respectively from compass solution method and inertial navigation solution method. At last, both simulations and ocean experiments verify the feasibility of the method.     

一种基于网络最大可控子图的导航搜索模型

基于网络可控性模型提出了最大可控子图的概念,在此基础上提出了一种基于最大可控子图的导航搜索模型. 模型中基于最大可控子图的加边策略用最小的代价解决了有向网络搜索中存在的粒子因“无路可走”而终止搜索的问题;基于最大可控子图部署导航节点,仅用节点总数2%左右的导航点,就使全网搜索时间接近导航网络的平均最短路径. 通过在ER和SF 网络上的实验表明,全网搜索时间与网络的可控性有关,可控性越好,添加的边数量越少,同时会使网络中导航节点分布越多,越能提高网络的搜索效率. 关键词： 导航搜索 有向网 网络可控性     

高强度二倍频激光辐照银薄膜靶的烧蚀和X光辐射实验研究

激光聚变物理实验中,背光透视照相是靶丸内爆动力学过程观测的重要方法. Ag是一种重要的背光材料, 激光辐照产生的等离子体可以产生强L线辐射, 研究其烧蚀和辐射特性, 对提高内爆靶丸背光透视照相的图像质量具有十分重要的意义.在神光II装置上, 采用第九路输出的2 ns, ～ 5× 10¹⁴ W/cm², 526.5 nm激光均匀辐照Ag薄膜靶, 实验研究了其烧蚀特性, 获得了银薄膜靶在激光烧蚀驱动下的飞行轨迹和飞行速度的数据. 实验结果与一维辐射流体力学模拟结果相符. 火箭模型对实验数据进行拟合, 得到了Ag材料的质量烧蚀速率和烧蚀压的数据. 采用平面晶体谱仪和X射线二极管探测器阵列观测等离子体的辐射特性, 获得了Ag等离子体辐射光谱和L线转换效率, 实验结果对激光聚变内爆靶丸背光照相的实验设计具有重要的参考价值.     

基于神光III原型装置的新型针孔点背光实验

在神光III原型装置上发展和改进了新型针孔点背光技术.通过1600 J/1 ns/351 nm激光与3μm钛背光靶相互作用产生4.75 keV的点光源,利用该点光源成像获得了高质量的钨丝以及靶丸图像,并通过多种诊断设备获取了较为完整的背光源参数.实验结果表明,新型的针孔点背光具备高亮度、高空间分辨等优点,可以广泛应用于高能量密度物理研究中.     

Simple-motion pursuit-evasion differential games,part 2: Optimal evasion from proportional navigation guidance in the deterministic and stochastic cases

The problem of the optimal evasion from a pursuer employing proportional navigation guidance is considered. Thus, we consider the problem of maximizing the time-to-capture when the problem parameters, namely, the speed ratio and the proportional navigation constant, are such that capturability of the evader is guaranteed.     

Computational efficiency and approximate inertial manifolds for a Bénard convection system

Summary A computational comparison between classical Galerkin and approximate inertial manifold (AIM) methods is performed for the case of two-dimensional natural convection in a saturated porous material. For prediction of Hopf and torus bifurcations far from convection onset, the improvements of the AIM method over the classical one are small or negligible. Two reasons are given for the lack of distinct improvement. First, the small boundary layer length scale is the source of the instabilities, so it cannot be modeled as a “slave” to the larger scales, as the AIM attempts to do. Second, estimates based on the Gevrey class regularity of solutions to the governing equations show that the classical and AIM methods may be virtually equivalent. It is argued that these two reasons are physical and mathematical reflections of one another.     

用Hadamard方法构造惯性流形

本文用Ｈａｄａｍａｒｄ方法为一类带有非线性项Ｒ：Ｄ（Ａ）→Ｈ的无限维耗散动力系统建立惯性流形．在建立惯性流形的过程中，系统的一种“不变锥性质”被充分利用着．这里，对惯性流形存在性至关紧要的谱间隙条件是．     

A biomagnetic method for studying gastro-intestinal activity

Summary A novel method to investigate the gastro-intestinal activity by means of a superconducting instrumentation based on SQUID sensors developed for biomagnetic measurements is presented. The magnetic field generated by a small marker ingested by the subject is measured over the abdomen. The localization of the marker,i.e. a magnetic dipole, is carried out by means of a standard algorithm used in biomagnetic studies. In this way it is possible to noninvasively study the activity of the gastro-intestinal system. This new approach may lead to important clinical applications.     

A double-stage piecewise recursive filter for real-time applications

This paper examines the basic problem of estimating the state of a system described by a set of dynamical equations. The state estimation is performed by means of optimal filtering techniques in which the state observation is given by a set of nonlinear equations.The basic issue encountered in most engineering problems is the availability of more observable information than the processor can effectively process in real-time, while performing full optimal filtering on all available observable data. To alleviate this deficiency, an algorithm is developed in which the rate of information processing is kept at a high value, while the system statistics are evaluated at a much slower rate.The method utilizes a combination of fast and slow filtering loops, in which the observable data are processed at a high rate during the fast loop, while the system error covariance, gain computations, and all other system statistics are processed at a lower rate in the slow loop. Methods are provided to resolve any incompatibility in the system statistics resulting from this fast-loop/slow-loop processing combination.Applications describing problems pertaining to aircraft navigation are presented. Specifically, applications to aircraft navigation through a satellite network are studied. Appropriate simulation results from the above studies are shown.This work was performed under contract with the Department of the Air Force, Space and Missile Organization (SAMSO), Los Angeles, California, Contract No. F04-701-75-C-0180.The authors are indebted to Dr. C. Johnson, GPS System Engineer, Mr. G. Consolver, GPS Software Manager, and Mr. W. Riley, Communications/Navigation Department, Texas Instruments for their continuous encouragement in the course of this work. Also, they are indebted to Major M. Birnbaum, SAMSO, for his constructive criticism on the conceptual design of this work, and to Mr. A. Bierman, Aerospace Corporation, for kindly providing simulation data of aircraft trajectories. Finally, the authors would like to express their gratitude to Dr. N. Carlson, Intermetrics, for valuable consultation during the progress of this work.Portions of this paper were presented by the senior author at the GSP Conference, Plan 76, IEEE Position, Location, and Navigation Symposium, San Diego, California, 1976.