变质心再入飞行器的质心移动方式研究

变质心控制是一种利用质量块的主动移动来改变飞行器质量特性的控制方式,该控制方式对于克服各种高速飞行器执行机构的气动烧蚀问题有着重要的意义.通过建立变质心再入飞行器的线性化方程,研究了质量块在飞行器内部不同方向上移动与可建立配平攻角之间的关系,并通过仿真计算可知再入飞行器再入的不同阶段质量块沿不同方向移动时的控制效率是有所差别的.研究结论对于提高变质心再入飞行器的控制效率有着重要的意义.     

科研工作的自组织过程及其政策启示

对工作对象的操控必须符合对象的性质或特点。从武警学院近三年的科研工作实践可以发现，要真正做好科研工作，使之进入良性循环，必须实现人为性与非人为性、有目的的组织性和科研系统自组织性的有机统一。这具有一般性的指导意义。     

有源雷达干扰弹干扰效能评估模型研究

针对信息化战场上有源雷达干扰弹的作战运用,应用模糊综合评判和AHP理论对其干扰效能评估进行研究。通过对该干扰弹干扰效能影响因素的分析,构造出干扰效能评估指标体系,采用AHP和征求专家意见确定了指标权重,经过对单因素的量化分析,得到了各影响因素隶属度的获取途径,并依此建立了二级模糊评估模型。该方法不仅能合理评估该雷达干扰弹的干扰效能,也对提高该弹的作战效能有一定指导作用。     

空袭兵器作战效能标准化问题研究

空袭兵器作战效能标准化将典型的空袭兵器的作战效能指数向选定的标准空袭兵器转化,其转化的结果用于防空兵力需求的计算。标准化过程主要包括标准空袭兵器的选择、作战效能指标体系的建立、指标权重的计算、性能指标参数的归一、效能指数的解算和标准化系数的换算六个步骤,运用加权算法、幂指数法和层次分析法建模计算,最终得出美台主要空袭兵器标准化效能数据。为空袭兵器作战效能的标准化提供了一种科学方法,从而便于实施防空作战资源需求分析和防空作战资源作战效能分析。     

基于益损分析的鱼雷战术效能的海洋环境影响评估

针对不同海洋环境中海水阻力系数和声线传播的变化特性,根据鱼雷航行及自导过程中的守恒原理,提出了一种评估海洋水文环境对鱼雷战术效能影响的新方法,并根据海洋水文环境对介质参数的影响,结合战术效能益损评价指标体系,建立了海洋环境对鱼雷战术效能影响的评估模型。通过仿真算例,对该评估方法进行了仿真实验,验证该方法的合理性和可靠性,进而发展运用于鱼雷作战使用的海洋环境影响评估和保障决策之中。     

太阳能热推进系统聚光器参数优化

采用先进遗传算法对太阳能热推进系统一次聚光器参数进行优化,达到减小推进系统质量的目的。以聚光器太阳光收集效率和聚光器质量为优化目标函数,建立聚光器工作的数学模型,并开展相关仿真研究。仿真结果表明,先进遗传算法可有效用于太阳光收集效率和聚光器质量优化分析。     

Damage of multi-layer spaced metallic target plates impacted by radial layered PELE

Three different kinds of PELE (the penetrator with lateral efficiency) were launched by ballistic artillery to impact the multi-layer spaced metal target plates. The impact velocities of the projectiles were measured by the velocity measuring system. The damage degree and process of each layer of target plate impacted by the three kinds of projectiles were analyzed. The experimental results show that all the three kinds of projectiles have the effect of expanding holes on the multi-layer spaced metal target plates. For the normal structure PELE(without layered) with tungsten alloy jacket and the radial layered PELE with tungsten alloy jacket, the diameters of holes on the second layer of plates are 3.36 times and 3.76 times of the diameter of the projectile, respectively. For radial layered PELE with W/Zr-based amorphous composite jacket, due to the large number of tungsten wires dispersed after the impact, the diameter of the holes on the four-layer spaced plates can reach 2.4 times, 3.04 times, 5.36 times and 2.68 times of the diameter of the projectile. Besides, the normal structure PELE with tungsten alloy jacket and the radial layered PELE whit tungsten alloy jacket formed a large number of fragments impact marks on the third target plate. Although the number of fragments penetrating the third target plate is not as large as that of the normal structure PELE, the area of dispersion of fragments impact craters on the third target plate is larger by the radial layered PELE. The radial layered PELE with W/Zr-based amorphous composite jacket released a lot of heat energy due to the impact of the matrix material, and formed a large area of ablation marks on the last three target plates.     

水下近场非接触爆炸载荷作用下加筋板毁伤变形的数值仿真研究

采用高动态非线性有限元程序MSC.Dytran对复杂加筋板结构在水下爆炸载荷下的动态响应和变形模式进行了仿真分析和模型试验,建立了复杂加筋板架结构水下爆炸作用下动态响应的有限元计算方法.研究了加筋板在水下爆炸载荷下的不同毁伤形式,并利用有限元程序对复杂毁伤形式进行了瞬态毁伤过程分析,认为一定药量近距离爆炸时局部破坏要先于整体破坏.     

Stage life testing

In progressive censoring, items are removed at certain times during the life test. Commonly, it is assumed that the removed items are used for further testing. In order to take into account information about these additional testing in inferential procedures, we propose a two‐step model of stage life testing with one fixed stage‐change time which incorporates information about both the removed items (further tested under different conditions) and those remaining in the current life test. We show that some marginal distributions in our model correspond either to progressive censoring with a fixed censoring time or to a simple‐step stress model. Furthermore, assuming a cumulative exposure model, we establish exact inferential results for the distribution parameters when the lifetimes are exponentially distributed. An extension to Weibull distributed lifetimes is also discussed.     

控制速度方向的弹道修正导引方法

由于制导炮弹由身管武器发射,其飞行控制能力和导引信息量有限,故基于预测落点位置偏差量来修正速度方向并在控制时间内连续分配导引指令的思想提出一种新的三维末制导方法。根据非线性弹道方程组的级数解预测弹丸落点位置,得到落点与目标的偏差,并提出两种通过此偏差解算当前速度方向修正量的方法。取剩余飞行时间为修正时间,通过将速度方向修正量分配到整个剩余导引段建立加速度修正公式,从而减小导引指令饱和的可能性。通过连续地预测落点和分配加速度指令来实时地导引飞行。仿真结果表明:该导引方法简单可行,精度高,对控制能力要求较低,且具备较好的制导效果和毁伤效果,可为该体制制导炮弹的应用提供参考依据。