标准误差的整体认识及运用

本文从物理量的测量角度出发,将标准误差在直接测量、间接测量、误差分析、结果处理等方面贯通一体,予以阐述和讲解,并综合了不同教材的不同说法,纠正了误差的不正确表示及概念上的模糊理解,从而建立起标准误差的整体认识和正确使用方法。     

超精密加工在线检测与误差补偿的理论与方法

超精密加工技术是高新技术、现代机械、电子产业以及国防工业的重要支柱,已成为技术发达国家重要的竞争目标。我系自１９８２年以来开展超精密加工技术的研究已有十多个年头了,取得了重要进展和重大突破。本文就所进行的研究工作,综合介绍了超精密加工中的若干理论与方法,包括形状误差在线检测的误差分离、误差补偿控制、微进给机构的非线性建模、微位移检测等内容,最后介绍了我系所取得的主要成果。     

C~3I系统中的哨所通讯网

本文提供了在C~3I系统中哨所通讯网的可行组网方案,从理论上分析了组网实践过程的各种因素。介绍了用信息机实现莫尔斯报务通讯中的困难和解决方法,并对如何提高报传通讯速率提出了探讨性意见。     

MIC总线多控制器通讯的设计与应用

MIC总线是专门为解决在恶劣环境下电力/数据的分配和管理而开发的一种具有高可靠性的现场控制总线。本设计实现了在MIC总线冗余系统中主控制器与从控制器间的数据通讯。在此基础上提出了MIC总线主/从控制器一致性的容错思想,并简要描述了该容错技术的实现过程。     

舰载火箭子母弹最优火力分配

舰载火箭子母弹对岸上目标实施火力压制射击时,火力分配方式直接影响毁伤效果和火力支援任务的完成.针对舰载火箭子母弹的射击特点,首先分析了海上射击误差,然后探讨了集群目标的简化处理方法,最后给出了最优火力分配时表尺差计算公式,并进行了举例分析.利用最优火力分配方法来计算舰载火箭子母弹效力射表尺差,避免了指挥员战场射击指挥的盲目性,可以在相同弹药消耗量情况下取得最佳射击效果,对未来舰载火箭子母弹的火力运用具有较高的现实意义.     

2(1/2)谱在直升机声信号特征提取中的应用

介绍了四阶累积量对角切片的一种定义,分析了其傅里叶变换(212谱)在提取三次相位耦合特征方面的良好性能及其估计方法;将其应用于具有三次相位耦合的直升机声信号特征提取。仿真结果表明,利用该方法能够分析信号的三次相位耦合信息,且具有计算方法简单、运算速度快及良好的抑制高斯噪声的优点。实际的数据处理结果验证了该方法的有效性。     

Matrix-geometric solution of discrete time MAP/PH/1 priority queue

We use the matrix-geometric method to study the discrete time MAP/PH/1 priority queue with two types of jobs. Both preemptive and non-preemptive cases are considered. We show that the structure of the R matrix obtained by Miller for the Birth-Death system can be extended to our Quasi-Birth-Death case. For both preemptive and non-preemptive cases the distributions of the number of jobs of each type in the system are obtained and their waiting times are obtained for the non-preemptive. For the preemptive case we obtain the waiting time distribution for the high priority job and the distribution of the lower priority job's wait before it becomes the leading job of its priority class. © 1998 John Wiley & Sons, Inc. Naval Research Logistics 45: 23–50, 1998     

坦克火控系统误差分析及仿真系统设计与实现

分析了坦克火控系统的误差源,并以误差分析问题为背景,设计并实现了一个仿真平台,并将其应用于火控系统设计过程中,为精度分配算法提供支持.仿真系统应用火控系统的基本数学模型,通过模拟实际射击来获得火控系统输入误差与输出误差的传递关系,以此分析各误差源对系统精度影响的敏感程度,帮助设计者选择影响较为显著的误差源来进行修正,从而获得较高的系统精度.     

大气湍流引起的相位起伏对相干态量子雷达相位估计的影响

基于马赫曾德干涉仪模型并采用相位扩散主方程描述大气相位起伏效应对量子雷达的影响,给出了光场在相位扩散通道的演化过程,详细分析了大气相位起伏对相干态宇称探测量子雷达相位估计分辨率和最佳灵敏度的影响,并计算了大气相位起伏下相位估计灵敏度的Cramer-Rao极限。研究发现:相位起伏对于分辨率的影响可通过增加单个脉冲平均光子数来消除。在强相位起伏情况下,宇称探测得到最佳灵敏度会严重偏离散粒噪声极限,但是在弱相位起伏情况下,通过与Cramer-Rao极限的对比,发现宇称探测是一种准最佳探测方案。     

Novel approach for active vibration control of a flexible missile

This paper investigates the feasibility of using an active dynamic vibration absorber (ADVA) for active vibration control of a flexible missile system through simulation. Based on the principles of a dynamic vibration absorber (DVA), a ring-type ADVA is first designed to attenuate the elastic vibration of the flexible missile, and the design of the active controller adopts the proportional-integral-derivative (PID) control algorithm. The motion equations of a flexible missile with an ADVA, which is subjected to follower thrust at its aft end, are derived using the Lagrangian approach. Taking the minimum of the root mean square (RMS) of the lateral displacement response of the center of mass as the objective function, a genetic algorithm (GA) is used to optimize the parameter of the DVA and PID controller. The numerical calculations show that the ADVA and DVA are effective in suppressing the vibration and provide approximately 41.2% and 17.6% improvement, respectively, compared with the case of no DVA. The ADVA has better performance than the DVA. When the missile is subjected to follower thrust, the effect of vibration reduction is more effective than the case without follower thrust. It is feasible to reduce vibration and improve the stability of flexible missiles by means of the ADVA.