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191.
《防务技术》2014,10(2):131-140
This paper deals with the issue of preparation of the aiming angles with the use of tabular firing tables and needed determination of the ballistic elements μB (ballistic wind wB, wxB, wZB, ballistic (virtual) temperature τB, ballistic density ρB) from the standardized met messages. The weighting factors are used for the calculation of ballistic elements μB that are incorporated into the trajectory calculations characteristics of weapon and ammunition. Two different methodologies practically used in the praxis are analysed and compared. For the comparison of the two methodologies the reference height of trajectory determined from the weighting factor functions is employed. On the basis of the analyses conducted, the potential for further increase in accuracy of these aiming angles preparation methods is pointed out. 相似文献
192.
针对未知环境下飞行器导航问题,提出一种基于视觉/惯导组合的测速测高方法。该方法构建包含前若干个成像时刻飞行器位置的惯导扩展状态方程,并采用一种基于摄像机两视图对极几何约束的线性视觉量测方程,通过卡尔曼滤波进行惯导速度修正,在此基础上利用多帧成像的立体视觉交会估计地面特征点坐标,进而得到飞行器相对高度。以飞行器典型巡航轨迹进行的仿真实验表明,该方法能够有效修正飞行器速度和相对高度误差,给出不随时间漂移的速度和相对高度测量结果,并很好地抑制飞行器位置误差的发散。 相似文献
193.
利用非线性模型预测控制(nonlinear model predictive control,NMPC)的思想建立了战机末端规避导弹的机动策略求解方法。根据导弹与战机的空战态势,建立了导弹与战机的相对运动微分方程;将导弹的导引律引入到导弹运动模型中,与飞机模型一起构建了系统预测模型,并对飞机和导弹的运动约束进行了分析。通过对导弹结构限制和战术特性的分析,给出了飞机机动规避导弹的性能指标,进而建立了机动规避导弹的最优控制模型。利用高斯伪谱法对模型进行求解,采用滚动优化策略实现了对机动规避策略的闭环求解。针对导弹气动参数和导航比未知以及相对测量量具有噪声的问题,利用极大似然法对导弹的气动参数和导航比进行估计,实现了对系统预测模型的反馈校正。仿真结果表明,此方法能够实现对导弹的机动规避。 相似文献
194.
针对运载火箭动力系统的性能评估,采用灰色关联分析模型有效解决了数据缺乏问题,并且利用层次分析法与离差最大化法组合确定指标权重,避免了使用单一赋权方法导致的主观性或者客观性不足的缺陷。最后,通过对国内外5种类型运载火箭的动力系统性能进行评估排序,对比数据结果表明,采用该方法能够对运载火箭动力系统性能进行合理的评估与排序,具有一定的应用价值。 相似文献
195.
196.
基于小波包分析的电磁导波信号缺陷识别 总被引:1,自引:0,他引:1
在钢管的电磁导波缺陷检测中,导波信号会不同程度地受到环境噪声污染。针对该问题,提出基于小波包系数区域相关分析的信号处理方法,通过对有缺陷与无缺陷情况的钢管电磁导波检测信号进行小波包分解重构、滤波和区域相关法对比分析,有效地解决了电磁导波检测中钢管缺陷的判别问题。 相似文献
197.
We study a class of new scheduling problems which involve types of teamwork tasks. Each teamwork task consists of several components, and requires a team of processors to complete, with each team member to process a particular component of the task. Once the processor completes its work on the task, it will be available immediately to work on the next task regardless of whether the other components of the last task have been completed or not. Thus, the processors in a team neither have to start, nor have to finish, at the same time as they process a task. A task is completed only when all of its components have been processed. The problem is to find an optimal schedule to process all tasks, under a given objective measure. We consider both deterministic and stochastic models. For the deterministic model, we find that the optimal schedule exhibits the pattern that all processors must adopt the same sequence to process the tasks, even under a general objective function GC = F(f1(C1), f2(C2), … , fn(Cn)), where fi(Ci) is a general, nondecreasing function of the completion time Ci of task i. We show that the optimal sequence to minimize the maximum cost MC = max fi(Ci) can be derived by a simple rule if there exists an order f1(t) ≤ … ≤ fn(t) for all t between the functions {fi(t)}. We further show that the optimal sequence to minimize the total cost TC = ∑ fi(Ci) can be constructed by a dynamic programming algorithm. For the stochastic model, we study three optimization criteria: (A) almost sure minimization; (B) stochastic ordering; and (C) expected cost minimization. For criterion (A), we show that the results for the corresponding deterministic model can be easily generalized. However, stochastic problems with criteria (B) and (C) become quite difficult. Conditions under which the optimal solutions can be found for these two criteria are derived. © 2004 Wiley Periodicals, Inc. Naval Research Logistics, 2004 相似文献
198.
A problem we call recurrent construction involves manufacturing large, complex, expensive products such as airplanes, houses, and ships. Customers order configurations of these products well in advance of due dates for delivery. Early delivery may not be permitted. How should the manufacturer determine when to purchase and release materials before fabrication, assembly, and delivery? Major material expenses, significant penalties for deliveries beyond due dates, and long product makespans in recurrent construction motivate choosing a release timetable that maximizes the net present value of cash flows. Our heuristic first projects an initial schedule that dispatches worker teams to tasks for the backlogged products, and then solves a series of maximal closure problems to find material release times that maximize NPV. This method compares favorably with other well‐known work release heuristics in solution quality for large problems over a wide range of operating conditions, including order strength, cost structure, utilization level, batch policy, and uncertainty level. Computation times exhibit near linear growth in problem size. © 2004 Wiley Periodicals, Inc. Naval Research Logistics, 2004 相似文献
199.
Parametric inference for component distributions from lifetimes of systems with dependent components
In system reliability analysis, for an n ‐component system, the estimation of the performance of the components in the system is not straightforward in practice, especially when the components are dependent. Here, by assuming the n components in the system to be identically distributed with a common distribution belonging to a scale‐family and the dependence structure between the components being known, we discuss the estimation of the lifetime distributions of the components in the system based on the lifetimes of systems with the same structure. We develop a general framework for inference on the scale parameter of the component lifetime distribution. Specifically, the method of moments estimator (MME) and the maximum likelihood estimator (MLE) are derived for the scale parameter, and the conditions for the existence of the MLE are also discussed. The asymptotic confidence intervals for the scale parameter are also developed based on the MME and the MLE. General simulation procedures for the system lifetime under this model are described. Finally, some examples of two‐ and three‐component systems are presented to illustrate all the inferential procedures developed here. © 2012 Wiley Periodicals, Inc. Naval Research Logistics, 2012 相似文献
200.
码相关参考波形(CCRW)技术以其设计灵活、抗多径性能优异等特点成为卫星导航多径抑制研究的热点,但目前相关文献在分析CCRW技术时常假设单边信道带宽无限或远大于扩频码率,且仅研究特定参考波形的性能,缺乏具有工程指导意义的定量结论.根据CCRW技术一般原理,推导了在无限带宽时任意参考波形的鉴别曲线计算公式,给出了满足稳定跟踪的波形约束条件.分析了不同带宽和闸宽参数的W2/W4/W5三类参考波形的准相干多径误差包络性能,仿真表明带限信道中W4、W5波形抗多径性能优于W2波形;以GPS L5和Galileo E5a/E5b的QPSK(10)信号为例进行原理样机试验,结果表明W2、W5算法比窄相关技术的3dB衰减多径误差包络面积减小达63%和72%.结论可用于现代化导航接收机的多径抑制设计. 相似文献