多旋翼无人机模型预测抗扰避障制导

多旋翼无人机的自主避障是完成复杂任务的基础,避障的效果直接影响无人机执行任务的效能。针对存在外部扰动的无人机避障问题,提出了一种基于模型预测的抗扰避障制导律设计方法。通过设计干扰观测器对系统动态中的外部干扰进行了估计,并基于李雅普诺夫函数方法设计辅助制导律用于建立稳定性约束条件。结合前两者与模型预测控制,在模型预测控制优化求解中考虑无人机与障碍物的关系,根据所设计的制导律求解水平线速度与偏航角速度指令实现无人机的避障。对所提出的避障制导律进行数值〖BHDWG8,WK10YQ,DK1*2,WK1*2D〗〖XCLQX.TIF;%129%129〗听语音 聊科研与作者互动 仿真和实物飞行验证,结果表明了所提方法的有效性。     

PAO8和45#变压器油基础油粘度调和及计算模型研究

采用高低温运动粘度测定仪测量PAO8(8#聚烯烃)合成基础油和45#变压器油基础油按不同比例调和后混合基础油的粘温性能,运用Arrhenius模型和Grunberg-Nissan模型计算混合基础油的理论粘度,研究粘度偏差率随测试温度的变化规律.实验结果表明:Arrhenius模型能准确预测混合基础油的高温运动粘度,粘度偏差率最大值不超过1%,而Grunberg-Nissan模型能精确计算混合基础油的低温运动粘度;PAO8和45#变压器油基础油调和能够获得高低温粘度的匹配.     

目标毁伤效果评估技术研究进展

目标毁伤效果评估作为目标保障的一项重要内容,对精确打击作战情报保障起到了核心作用,是现代精确打击体系的一个重要环节和关键步骤。文章从评估方法、评估模型和评估系统三个方面入手,梳理了国内外目标毁伤效果评估技术的最新研究进展,并对目前各类评估方法、模型及系统的优缺点分别进行了评述。最后,指出了该领域今后的研究方向。     

基于正态云模型和信息公理的设计评价方法

设计方案的选择和评价是产品设计过程中的一个重要环节,就此环节提出了一种基于正态云模型和公理化设计理论中信息公理的设计方案评价方法。该方法运用正态云模型和信息公理将定性的模糊信息数值化,通过计算求得设计中各个指标的信息量以及各个设计方案的信息总量,通过比较各个方案的信息总量大小来对设计方案进行评价。以某型油料加注装备设计评价为例,证明了此方法的有效性。     

弹药物资储备布局规划仿真模型＊

介绍了当前弹药物资储备布局规划的现状,对其涉及的要素进行分析,构建了弹药物资储备布局规划网络模型。在此基础上提出了分析模型,将弹药物资布局规划求解问题描述为有约束条件的多目标优化数学模型,解决了各仓库弹药存储量难以预测的问题,并通过实验进行了验证分析。     

基于模型概率估计的两层交互多模型算法

在机动目标跟踪问题的研究中,针对转弯机动目标跟踪精度差的问题,设计了一种利用模型概率对模型集合进行实时计算的两层交互多模型算法。该算法由第一层目标转弯速率的粗估计和第二层目标状态向量的精估计构成,它利用第一层模型计算出的目标运动估计转弯速率,构建与当前目标运动状态匹配程度较高的第二层转弯模型集合,并将该转弯模型集合运用于状态估计中。仿真结果证明了该算法在针对转弯机动目标时仍有较好的跟踪精度。     

基于时滞兰彻斯特战斗模型的现代攻防对抗?

针对现代攻防对抗研究的复杂性,在分析已有的现代战争模型的基础上,充分考虑时间因素在作战中的影响,建立了反映双方对抗态势的时滞兰彻斯特战斗模型,并借助Matlab?Simulink工具箱,对模型进行了数值仿真实验。仿真结果表明：时间因素在现代攻防对抗中占据越来越重要的地位。最后依据所得结论,分别探讨了攻防双方为取得最佳战绩应当采取的对策,为武器装备发展规划、现代作战决策与军事练兵提供一定的理论指导。     

基于SQP法的助推-滑翔导弹助推段弹道优化研究

轨迹优化是飞行器总体优化设计中的重要组成部分,它贯穿于飞行器的整个设计过程。高超声速助推-滑翔导弹的弹道优化问题涉及攻角、法向过载、最大动压等多种约束条件,是一种复杂的最优控制问题。序列二次规划法（SQP）是解决该类问题行之有效的数值优化方法。本文利用SQP算法对助推-滑翔导弹助推段进行弹道优化,为这一高超声速飞行器的整体结构设计提供了有益的参考。     

Long-rod penetration: the transition zone between rigid and hydrodynamic penetration modes

Long-rod penetration in a wide range of velocity means that the initial impact velocity varies in a range from tens of meters per second to several kilometers per second. The long rods maintain rigid state when the impact velocity is low, the nose of rod deforms and even is blunted when the velocity gets higher, and the nose erodes and fails to lead to the consumption of long projectile when the velocity is very high due to instantaneous high pressure. That is, from low velocity to high velocity, the projectile undergoes rigid rods, deforming non-erosive rods, and erosive rods. Because of the complicated changes of the projectile, no well-established theoretical model and numerical simulation have been used to study the transition zone. Based on the analysis of penetration behavior in the transition zone, a phenomenological model to describe target resistance and a formula to calculate penetration depth in transition zone are proposed, and a method to obtain the boundary velocity of transition zone is determined. A combined theoretical analysis model for three response regions is built by analyzing the characteristics in these regions. The penetration depth predicted by this combined model is in good agreement with experimental result.     

Experiment and simulation of launching process of a small-diameter steel cartridge case

In order to explore the rules of the deformation force during the launching of a small-diameter steel cartridge, the semi-closed bomb test method is used to test the greatest strains on chamber outer wall under the different chamber pressures. The pressure curves of cartridge chamber are measured in experiment, and the tensile test data of cartridge are loaded into the numerical calculation to compare with the experimental data. The conclusion was obtained that the calculated results match better with the experimental results by considering strain rate bilinear kinematic hardening material constitutive model. The forces on the various parts of the cartridge during launching and their deformation rules are achieved, in which the equivalent plastic strain decreases and the cylinder ring withstands the maximum equivalent stress when the cartridge case clings to the bore from the mouth to the bottom.