直升机野战油料保障模拟优化研究

野战条件下,场站通常在前沿阵地开设野战直升机场实施伴随保障,其中油料保障主要采取飞机加油车先对直升机实施加油,后到野战机场油库领取油料这一方式进行。若将野战直升机场油料保障作为一个系统来研究,要实现适时、适量的油料保障,确定合适的飞机加油车及野战机场油库发油鹤位数量是一个关键问题。利用GPSSW语言对这一问题进行模拟,得出模拟结果并进行统计分析,经反复模拟和参数比较得到适合的参数,为部队保障提供依据。     

军队油料运输网络安全优化研究

军队油料运输路径选择受交通运输网络和运输线路风险的影响和制约。战时,交通运输网络是敌方破坏的重点,油料运输面临很大风险,安全形势非常严峻。合理优化交通运输网络,选择合适的运输路径是避免敌方破坏、保障油料运输安全的重要途径。从不同决策角度出发,选择以总后勤部军事交通运输部为代表的网络规划者和以各级军事代表处及运油分队为代表的运输路径选择者为两级决策者,以实现总体风险均衡和单条运输路径目标最优为出发点,建立双层规划模型,对运输网络进行优化,选择最优运输路径。该法既可降低不同性质的风险,又能兼顾各种风险的相互影响。     

某型跳频电台故障定位系统设计与实现

文章介绍了针对某型跳频电台的故障定位系统,该系统以计算机和虚拟仪器技术为核心,通过设计测试平台实现板卡分离,并根据板卡特点设计自动快速检测和辅助测试准确定位功能,能够将故障锁定到具体元器件。该系统定位故障速度快、结果准确、性能稳定,并已成功应用于某测试任务,有较好的工程应用价值。     

并联机构奇异点的运动分岔研究

采用静态分岔理论研究一般并联机构在奇异点处的运动分岔现象。通过约束方程研究了几种简单机构在驱动奇异和末端执行器奇异下的不同分岔类型,并研究了机构参数对分岔性态的影响。指出非持久性奇异分岔可以通过调整机构参数转换为持久性奇异分岔,从而克服机构在奇异点邻域内的运动不确定性。     

小型地面机器人链路通信距离测试方法设计

针对复杂环境条件下小型地面机器人链路通信距离测试方法问题,分析并指出了传统链路通信距离测试方法无法适用于地面机器人测试的原因,根据小型地面机器人使用环境和无线链路近地传播特点,选取对数距离路径损耗模型改进了传统测试方法,并在3种典型环境下进行了实地测试验证,结果表明:新方法能通过定量数据揭示被测机器人在不同环境下链路通信环境的差异性,适用于复杂环境下小型地面机器人链路通信距离测试.     

电磁炮炮管振动信号分析及处理方法

炮管发射振动是影响电磁炮发射稳定性及射击精度的关键因素,获取炮管振动信号有效数据,对优化其发射性能具有重要的意义.在对电磁炮炮管振动信号分析的基础上,提出了采用小波阈值去噪和最小二乘法相结合的信号处理方法来去除振动干扰信号,通过仿真实验,理论验证了该信号处理方法的有效性;设计测试系统进行振动实测实验,并使用该信号处理方法获得振动有效信号,进一步验证了该方法的有效性和实用性;计算得到炮管振动位移参量,为电磁炮设计、优化提供了理论依据.     

Research on the influences of confining pressure and strain rate on NEPE propellant: Experimental assessment and constitutive model

In order to study the influences of confining pressure and strain rate on the mechanical properties of the Nitrate Ester Plasticized Polyether (NEPE) propellant, uniaxial tensile tests were conducted using the self-made confining pressure system and material testing machine. The stress-strain responses of the NEPE propellant under different confining pressure conditions and strain rates were obtained and analyzed. The results show that confining pressure and strain rate have a remarkably influence on the mechanical responses of the NEPE propellant. As confining pressure increases (from 0 to 5.4 MPa), the maximum tensile stress and ultimate strain increase gradually. With the coupled effects of confining pressure and strain rate, the value of the maximum tensile stress and ultimate strain at 5.4 MPa and 0.0667 s⁻¹ is 2.03 times and 2.19 times of their values under 0 MPa and 0.00333 s⁻¹, respectively. Afterwards, the influence mechanism of confining pressure on the NEPE propellant was analyzed. Finally, based on the viscoelastic theory and continuous damage theory, a nonlinear constitutive model considering confining pressure and strain rate was developed. The damage was considered to be rate-dependent and pressure-dependent. The constitutive model was validated by comparing experimental data with predictions of the constitutive model. The whole maximum stress errors of the model predictions are lower than 4% and the corresponding strain errors are lower than 7%. The results show that confining pressure can suppress the damage initiation and evolution of the NEPE propellant and the nonlinear constitutive model can describe the mechanical responses of the NEPE propellant under various confining pressure conditions and strain rates. This research can lay a theoretical foundation for analyzing the structural integrity of propellant grain accurately under working pressure loading.     

An experiment evaluating how the tiny mass eccentricities in spin-stabilized projectiles affect the position of impact points

This study investigates and quantifies some possible sources affecting the position of impact points of small caliber spin-stabilized projectiles (such as 12.7 mm bullets). A comparative experiment utilizing the control variable method was designed to figure out the influence of tiny eccentric centroids on the projectiles. The study critically analyzes data obtained from characteristic parameter measurements and precision trials. It also combines Sobol's algorithm with an artificial intelligence algorithm—Adaptive Neuro-Fuzzy Inference Systems (ANFIS)—in order to conduct global sensitivity analysis and determine which parameters were most influential. The results indicate that the impact points of projectiles with an entry angle of 0° deflected to the left to that of projectiles with an entry angle of 90°. The difference of the mean coordinates of impact points was about 12.61 cm at a target range of 200 m. Variance analysis indicated that the entry angle — i.e. the initial position of mass eccentricity — had a notable influence. After global sensitivity analysis, the significance of the effect of mass eccentricity was confirmed again and the most influential factors were determined to be the axial moment and transverse moment of inertia (Izz Iyy), the mass of a projectile (m), the distance between nose and center of mass along the symmetry axis for a projectile (Lm), and the eccentric distance of the centroid (Lr). The results imply that the control scheme by means of modifying mass center (moving mass or mass eccentricity) is promising for designing small-caliber spin-stabilized projectiles.     

助推-滑翔式导弹中段弹道方案的初步分析

建立了助推—滑翔式弹道中段的无量纲运动方程。采用非线性规划方法实现弹道优化。首先求解不同初始速度、速度倾角和最大升阻比的最大射程弹道,然后考虑驻点热流、过载约束,求解总气动加热最小和射程最大的最优弹道。基于前者的计算结果分析了初始条件对最大射程弹道的影响。将考虑约束的再入滑翔弹道与弹道式再入的特征参数比较,表明再入滑翔弹道的峰值热流较小,而总气动加热增加,但再入滑翔飞行时间在一般锥形体再入机动飞行器的热防护系统可承受的时间范围内。     

油库安全事故致因机理及安全评价方法研究

首先基于油库安全和事故状态分析,将油库安全事故的影响因素分为人的行为、物的状态、管理和环境四个要素,提出油库安全事故致因新模式,即两种安全模式和一种事故致因模式,以从源头上控制油库事故的发生。其次,依据致因模式,建立了油库安全状况评价指标体系,包括人员、装(设)备、材料、环境、方法,有助于评判油库安全状况。最后,依据安全事故新模式和安全评价指标体系,提出了油库安全保障体系,包括安全教育、安全技术培训、安全法规、安全监督、安全预案与救援、安全设施建设等体系。