机载雷达空地状态的工程实践

从５０年代末到今天,机载雷达的空地状态在国外已经广泛地应用于多种机载火控系统之中,这对于提高机载武器对地攻击的效能以及载机应付多种作战环境的能力,均有显著功效。而这个状态的应用在我国却是一项空白。本文在于介绍空地状态的原理及对测距误差的分析。还叙述了在研制及试飞中存在的一些实际问题,以期待同行们共同探讨,并能推动此项技术在国内机载火控系统中的应用。     

铝合金表面涂覆隐身吸波涂层脱落原因分析

通过对某装备车体外脱落隐身吸波涂层样品的表面形貌、截面形貌、元素组成及含量分析,发现吸波涂层和Al2O3钝化层之间没有化学结合键,只存在物理吸附和机械结合,在外部环境的作用下,很容易引起隐身吸波涂层的脱落。     

Military Off the Shelf Procurements: A Norwegian Case Study

Buying off the shelf procurements (OTS) has become an important part of the national acquisition strategy in several countries, and this paper seeks to bring empirical evidence on OTS as the preferred acquisition strategy by use of data from 2015 to 2022 investment portfolio of the Norwegian Armed Forces. We develop definitions for three categories of procurement – OTS, modified OTS and development projects – as well as a method to classify projects into these categories. Our first finding is that the characteristics of OTS projects correspond to modified OTS and development projects. Our second finding indicates that OTS projects perform better when it comes to the completion of projects according to the initial schedule, compared to development projects.     

应用交互多模(IMM)算法跟踪低空目标

雷达跟踪低空目标时,由于多路径传播的影响,目标俯仰角的测量会出现测量误差.并且由多路径传播引起的测量噪声方差较大,在时间上具有相关性.应用交互多模(IMM)算法来提高跟踪低空目标的性能,并且提出了一种去相关的滤波方法来克服多径误差相关性的影响,最后给出了计算机仿真的滤波结果.     

Production to order and off‐line inspection when the production process is partially observable

This study combines inspection and lot‐sizing decisions. The issue is whether to INSPECT another unit or PRODUCE a new lot. A unit produced is either conforming or defective. Demand need to be satisfied in full, by conforming units only. The production process may switch from a “good” state to a “bad” state, at constant rate. The proportion of conforming units in the good state is higher than in the bad state. The true state is unobservable and can only be inferred from the quality of units inspected. We thus update, after each inspection, the probability that the unit, next candidate for inspection, was produced while the production process was in the good state. That “good‐state‐probability” is the basis for our decision to INSPECT or PRODUCE. We prove that the optimal policy has a simple form: INSPECT only if the good‐state‐probability exceeds a control limit. We provide a methodology to calculate the optimal lot size and the expected costs associated with INSPECT and PRODUCE. Surprisingly, we find that the control limit, as a function of the demand (and other problem parameters) is not necessarily monotone. Also, counter to intuition, it is possible that the optimal action is PRODUCE, after revealing a conforming unit. © 2007 Wiley Periodicals, Inc. Naval Research Logistics, 2007     

一种稳健的循环平稳信号时延估计算法

基于信号循环平稳特性的时延估计算法具有较强的抗干扰和抗噪声能力,但循环频率误差时性能下降严重。针对这一问题,首先分析了循环频率误差对循环时延估计算法中,循环互相关函数相关法估计性能的影响,进而提出了一种对循环频率误差稳健的改进循环时延估计算法。改进算法通过两次搜索确定循环频率的真实值。仿真实验结果表明,改进算法可以有效地校正循环频率误差,最终使时延估计误差与无循环频率误差时基本相同。     

舰炮一维弹道修正弹射击误差分离和校正研究

由于工作原理不同,传统无控弹射击校正方法不适用于一维弹道修正弹。分析了舰炮使用一维弹道修正弹射击误差构成和射击观测特点,提出一维弹道修正弹射击校正新方法,首先通过修正机构不工作,利用观测弹着点相对预测弹着点偏差平均值校正火控设备预测弹着点误差;然后利用修正弹正常工作时观测弹着点相对目标（或提前点）偏差平均值校正修正机构误差。假设各误差值,通过解弹道方程仿真计算表明,按新方法射击校正能够显著提高射击精度。     

信息错误检测项目的关系分析

从提高信息质量这一目标入手,定义了理论信息错误类别空间、可检测信息错误类别空间、检测项目集等基础概念,分析了检测项目集之间的对等、相交、包含和互斥等4种关系及其特点,形成了信息错误检测项目集的2种生成与优化方式,以及若干优化原则,并给出各原则的优先顺序。     

THE F‐35 JOINT STRIKE FIGHTER AS A SOURCE OF INNOVATIon AND EMPLOYMENT: SOME INTERIM RESULTS

The F‐35 Joint Strike Fighter (JSF) programme is important for innovation in the Dutch economy and also contributes to other programmes in the aerospace industry (spin‐off) and other industries (spillover). On top of the expected value of US$9.2 billion in development and production, based on interviews with 10 companies and research institutes, an expected spin‐off of US$1.1 billion and an expected spillover of US$120 million will result. In addition, over 23,000 man‐years are associated with the activities in the development and production of the JSF. This study excludes the large and labour‐intensive Maintenance, Repair and Overhaul (MRO) activities. Further validation of data and an update of current results is planned for 2006.     

弹道修正弹射程偏差预测与阻力板展开时机优化

根据弹道修正弹阻力板的展开控制对于射程偏差预测要求的实时性,提出基于摄动原理的射程偏差预测算法.为解决阻力板修正能力在线计算数据量大的问题,提出在弹载计算机上装定阻力板修正能力表格的方法,给出发射前计算修正能力表格的过程和飞行中使用修正能力表格的步骤,提出阻力板展开时机的优化判断条件,并采用该方法对某型弹道修正火箭弹射程修正控制进行仿真试验和飞行试验.仿真试验结果表明,当目标射程为33 565.4m时,经修正后火箭弹的射程偏差能控制在20m以内;飞行试验结果表明,弹道修正火箭弹的射程偏差实测为24m,射程精度得到明显提高.