载机扰动下SAR/GMTI旋转目标微多普勒特性分析

目标微动部件激励的雷达微多普勒信号稳定而独特,反映了该目标的本质特征。针对采用相位中心偏置技术(DPCA)的SAR/GMTI系统,研究存在载机扰动下的旋转目标的微多普勒特性。构建飞行平台与微动目标的几何模型,推导旋转目标的微多普勒信号模型,分析典型的载机纵向扰动对微多普勒时频特性构成的影响;并通过仿真实验,验证了上述理论分析的正确性。     

基于DOB和二自由度控制器的某火炮稳定控制系统设计

火炮稳定控制系统性能会受到如路况、火炮射击时产生的冲击力矩等外部扰动以及摩擦力矩变化、测量噪声、转动惯量变化等内部参数摄动的影响。针对此问题,引入一种DOB观测器和二自由度控制算法,来减少摩擦对系统性能的影响,提高系统对载体扰动的隔离能力。仿真和实验结果表明,所提出的算法可以有效提高系统的稳定精度和速度伺服性能。     

Interface defeat studies of long-rod projectile impacting on ceramic targets

The interface defeat phenomenon always occurs when a long-rod projectile impacting on the ceramic target with certain velocity, i.e., the projectile is forced to flow radially on the surface of ceramic plates for a period of time without significant penetration. Interface defeat has a direct effect upon the ballistic performance of the armor piercing projectile, which is studied numerically and theoretically at present. Firstly, by modeling the projectiles and ceramic targets with the SPH (Smoothed Particle Hydrodynamics) particles and Lagrange finite elements, the systematic numerical simulations on interface defeat are performed with the commercial finite element program AUTODYN. Three different responses, i.e., complete interface defeat, dwell and direct penetration, are reproduced in different types of ceramic targets (bare, buffered, radially confined and oblique). Furthermore, by adopting the validated numerical algorithms, constitutive models and the corresponding material parameters, the influences of projectile (material, diameter, nose shape), constitutive models of ceramic (JH-1 and JH-2 models), buffer and cover plate (thickness, constraints, material), as well as the prestress acted on the target (radial and hydrostatic) on the interface defeat (transition velocity and dwell time) are systematically investigated. Finally, based on the energy conservation approach and taking the strain rate effect of ceramic material into account, a modified model for predicting the upper limit of transition velocity is proposed and validated. The present work and derived conclusions can provide helpful reference for the design and optimization of both the long-rod projectile and ceramic armor.     

An investigation on anti-impact and penetration performance of basalt fiber composites with different weave and lay-up modes

The woven basalt fiber composites (WBFC) and the unidirectional [0°/90°/45°/-45°]_s basalt fiber composites (UBFC) were prepared by hot-pressing. Three-point bending test, low velocity impact test, and ballistic test were performed to the prepared composites. After the tests, the specimens were recovered and analyzed for micromorphology. Three-point bending tests show that both the bending strength and stiffness of the WBFC surpass those of the UBFC. Low velocity impact test results show that the low velocity impact resistance to hemispherical impactor of the UBFC is higher than that of the WBFC, but the low velocity impact resistance to sharp impactor of the UBFC is lower than that of the WBFC. For the ballistic test, it can be found that the ballistic property of the UBFC is higher than that of the WBFC. After the tests, microscopic analysis of the specimens was applied, and their failure mechanism was discussed. The main failure modes of the UBFC are delamination and fibers breakage under the above loading conditions while the main failure mode of the WBFC is fibers breakage. Although delamination damage can be found in the WBFC under the above loading conditions, the degree of delamination is far less than that of the UBFC.     

飞机反区速度矢量不稳定及其控制的机理

在信号流图的基础上,提出多回路分析的方法,并用于研究反区时速度矢量不稳定及其稳定控制的机理。建立了纵向动力学的信号流图,并证明了一个回路的收敛性定理。在此基础上,通过理论分析得出了速度矢量不稳定在不同层面上的原因,也得出了速度和轨迹的发散度表达式等,并表明阻力-速度曲线、轨迹角-速度曲线、极曲线、阻力系数曲线等存在相互对应的反区和正区,并且阻力-速度曲线和轨迹角-速度曲线在斜率上成比例。研究得出进场动力补偿系统下速度矢量的稳定临界条件、收敛度、稳定机理等,理论分析和仿真比较了速度恒定进场动力补偿系统和迎角恒定进场动力补偿系统在控制性能上的差异。     

卫星活动部件的干扰辨识与抑制

采用干扰辨识的方法实现带活动部件三轴稳定卫星的高精度姿态控制问题.首先以扫描镜为例进行,分析扫描镜运动对卫星产生的等效干扰力矩;然后根据卫星控制系统的稳态输出数据,采用特征系统实现算法对扫描运动产生的干扰频率进行闭环辨识;最后在所辨识干扰频率的基础上,采用偶极子干扰抑制滤波器消除扫描镜运动干扰对卫星姿态的影响.仿真结果表明,所提出的方法能有效地克服活动部件运动产生的未知干扰对卫星姿态稳定度的影响,提高在轨运行卫星的姿态控制精度.     

群体性事件情报预警困境的博弈分析

在公安边防部门辖区内,群体性事件时有发生,成为影响辖区治安的主要因素。如何基于所掌握的情报,找出一种科学合理的情报分析方法成为边防部门亟待解决的问题。从博弈论的角度,建立模型,用数学方法进行求解,对公安边防部门与群体性事件的策动者进行博弈分析。     

弹丸速度的数字化激光幕测试技术

针对传统弹丸速度测量方法的局限,提出一种新的弹丸速度测试技术——数字化激光幕结合互相关速度测量算法的测试技术,并给出了激光总体测速方案、测速原理以及互相关测速方法,经靶场试验验证测试效果良好。     

差压式管道内检测机器人驱动力与速度分析

差压式管道内检测机器人是利用管道中流动介质压力差驱动的检测装置,机器人受力情况及周围流场分布对其运动状态有着重要的影响。通过对检测机器人受力分析和数值模拟,讨论了影响给定机器人驱动力的主要因素,得到了以水为流动介质在水平管道情况下,水流速度与机器人稳态速度的近似关系式,为以后进一步研究机器人定位提供帮助。     

群体性事件参与者的社会心理特征探析

现阶段我国群体性事件逐渐成为影响社会稳定的重要问题.群体性事件参与者普遍的失衡心理、自认为行为＂合理＂的片面心理、侥幸投机心理和易受感染的从众心理是酿成群体性事件的重要社会心理特征.加强心理疏导是预防和处置群体性事件的重要措施之一.