C~3I 系统多传感器的信息融合——Fuzzy 函数聚类算法

在对多类传感器收集空中目标状态信息描述的基础上,用Ｆｕｚｚｙ目标函数聚类算法建立了对空情数据融合的数学模型。对数据融合过程,参数的初始化问题进行了实际应用的讨论;并对其应用效果和优势作了实际的分析。该方法是Ｃ３Ｉ系统数据融合技术的有效方法之一。     

介子跃迁形状因子的重夸克极限和1/m_Q修正

在BS理论框架下,对0~-→0~-和0~-→1~-(0~-和1~-分别代表赝标介子和矢量介子)跃迁的形状因子进行模型无关的分析.结果表明BS框架既能给出重夸克极限下的自旋—味对称性,又能给出重夸克有效理论关于1/m_Q修正的Luke定理及其它关系.     

C~3I系统的决策时延分析

决策是C~3I 系统的核心问题之一。用Petri 网理论研究C~3I 系统的决策问题已取得了长足的进展。根据决策过程各阶段之所需时间具有随机性及不独立性的特点,以变迁发射时间不独立的随机Petri 网作为决策时延的建模与分析工具,并给出了这种随机Petri 网模型的一般分析方法。     

C3I系统仿真评价环境与方法研究

C3I系统是一个复杂的大系统,如何有效地分析、研究和评价C3I系统的效能一直是C3I系统研究领域里的一个难点.仿真技术的出现为分析和评价C3I系统效能提供了一种新的手段.该文在分析基于仿真的C3I系统效能评价过程的基础上,设计实现了基于分布交互仿真技术的"C3I系统仿真评价环境",对仿真评价环境的体系结构、仿真技术体制等关键问题进行了论述.利用该环境可以对C3I系统作仿真分析、性能指标对比分析以及作战效能分析.由于仿真试验只是获取评价系统所需数据的一种手段,文章最后对几种常用的系统综合评价方法进行了探讨.     

Probabilistic analysis of an asymptotically optimal solution for the completion time variance problem

Scheduling a set of n jobs on a single machine so as to minimize the completion time variance is a well‐known NP‐hard problem. In this paper, we propose a sequence, which can be constructed in O(n log n) time, as a solution for the problem. Our primary concern is to establish the asymptotical optimality of the sequence within the framework of probabilistic analysis. Our main result is that, when the processing times are randomly and independently drawn from the same uniform distribution, the sequence is asymptotically optimal in the sense that its relative error converges to zero in probability as n increases. Other theoretical results are also derived, including: (i) When the processing times follow a symmetric structure, the problem has 2^{⌊(n−1)/2⌋} optimal sequences, which include our proposed sequence and other heuristic sequences suggested in the literature; and (ii) when these 2^{⌊(n−1)/2⌋} sequences are used as approximate solutions for a general problem, our proposed sequence yields the best approximation (in an average sense) while another sequence, which is commonly believed to be a good approximation in the literature, is interestingly the worst. © 1999 John Wiley & Sons, Inc. Naval Research Logistics 46: 373–398, 1999     

聚钛碳硅烷的新合成法及其研究

从聚硅烷(PS)与钛酸丁酯。(Ti(OBu)_4)出发,不采用任何反应促进剂直接合成了含钛碳化硅纤维的先驱体聚钛碳硅烷(PTC)。在这一反应中,PS 首先裂解成含Si—C 骨架与Si—H 键的低分子聚硅烷(LPS)。然后,由LPS 中的Si—H 键与Ti(OBu)_4的反应以及LPS 的Si—Si 骨架裂解转化为Si—C 骨架的反应制得了PTC.本文对这种新合成法所涉及的反应过程进行了研究,并比较了新旧两法得到的PTC—1与PTC—Ⅱ的结构异同,报告了以新法制得的PTC—Ⅱ为先驱体得到的含钛碳化硅纤维的优良性能。     

有人/无人平台协同技术与行动模式研究

无人平台已广泛用于军用和民用市场,并在反恐、维稳、排爆,侦察等领域发挥了极其重要的作用。目前已形成了有人/无人平台共同协作完成任务的工作模式,大大地提高了工作的时效性、适应性、作战效能等。为了提高有人/无人平台的协同作战能力,本文研究有人/无人平台的协同作战技术体系以及作战模式,以解决在协同侦察、搜救、监视等应急任务中遇到的各种问题。此外,提出了一套完整的协同作战想定,可用于有效验证相关的协同技术。     

Parametric study of single confined fragment launch explosive device

In this article, parametric study of single confined fragment launch device was carried out. The configuration proposed was further studied to derive the empirical relationship for effect of fragment size, charge size, confinement thickness on fragment velocity. The simulations were carried out using ANSYS-AUTODYNE explicit solver. Fragment velocities were estimated as a function of different parametric combinations of explosive quantities, charge length to diameter ratio, fragment height to diameter ratio, confinement thickness, fragment material and fragment mass. The data was further converted to charge to metal ratio under fragment and confinement. It was observed that, increase in confinement thickness, charge quantity and decrease in fragment height increases the fragment velocity. It is also noted that, charge to metal mass ratio under fragment significantly affects the fragment velocity. At the end, an empirical relationship for fragment velocity interms of all these parameters was established. Using these relations, two velocities 1831.92 m/s and 2523.9 m/s required for NATO STANAG 4496 IM test were estimated. The design parameters for these velocities are presented. Also, the results estimated using the empirical relationship has been compared with published experimental data. Error in the predicted velocities is within the acceptable range. The empirical relationship proposed will be useful for finalization of design of the fragment launch device.     

电磁轨道发射中内弹道动力响应特性分析

将轨道简化为移动载荷作用下固定在弹性支撑上的Bernoulli-Euler梁,通过静态电磁-结构耦合有限元模型求得外围封装的等效刚度,计算得到发射器的临界速度。另外,利用混合有限元/边界元法建立电磁-结构-运动多物理场耦合的动力学模型,求得枢轨动态接触压力和轨道的应力应变分布特性。通过在轨道背面布置光纤光栅应变传感器,利用测量数据验证了动力响应特性,并分析了弹丸在内弹道的稳定性。针对典型30 mm × 30 mm矩形口径发射器,分析及试验结果表明：C型电枢对轨道的电磁挤压力在平顶沿起始时刻达到最大值,之后随着时间推移逐渐减小;电枢通过引起的应力波在高速段容易与轨道中反射应力波发生共振,并且轨道在电枢运动的中间高速段区域受力最为集中,应力集中水平约是起始低速段区域的2.44倍;电枢运动高速段会出现晃动现象,进而引起上下轨道受力的不对称性。分析及试验结果对研究电磁轨道发射器内弹道动力响应特性和发射器结构设计具有重要指导意义。     

新体制导航信号下I/Q幅相不一致对接收机测距零值的影响分析

随着现代化导航信号带宽的增大,由于可以大幅降低采样率,复信号采样的优势日趋明显。由于存在I/Q幅相误差,复信号采样对导航接收机伪距测量造成了一定影响。改进了信道非理想与I/Q幅相误差共同影响BPSK/QPSK信号零值测量的分析模型;在该模型基础上,推导得到了任意I/Q误差和信道非理想特性影响BOC信号伪距零值的模型;探讨了二者在频域抗干扰应用场景下引起的零值变化;理论分析与软件接收机仿真结果高度吻合,误差在1.5×10^-4码片内,证明了分析模型的精确性。该分析方法可用于对高性能导航接收机信道特性进行事先约束及筛选,以确保干扰场景下的零值变化满足要求。