分布式多目标跟踪中的数据融合问题——一种新的相容性准则及融合过程分析

用一个新观点讨论了利用分布式传感器网络进行多目标跟踪中出现的信息融合问题。对航迹相容性和假设相容性的判别问题 ,从一个新的观点 ,即“无矛盾原则”出发 ,给出了完整的与前人不同的航迹和假设相容性的判别条件。同时对航迹的融合过程和假设的融合过程做了详细的分析 ,证实两个假设相融合得到多个全局假设是合情合理的     

子母弹再入段飞行干扰弹道仿真系统设计与实现

建立了分块的子母弹全弹道仿真流程,给出了影响子母弹子弹落点散布的三类再入段干扰因素,并提出了干扰因素的基本分析方法,最后对子母弹再入段飞行干扰弹道仿真系统的设计方案进行了总结。结果表明,该仿真系统可以弹道的不同阶段为入口进行不同导弹飞行段的弹道解算,通过设置不同的干扰因素,可进行多因素对子弹落点散布影响研究,为子母弹子弹落点散布规律的研究提供技术支撑。     

The Obama administration's phased-adaptive architecture: technological,operational and political issues

In 2009, the Obama administration announced a new missile defense strategy, termed a phased-adaptive architecture (PAA) focused primarily on countering the growing threat from theater ballistic missiles. The success of this strategy is predicated on the rapid development and fielding of successive increments of defensive capability in a manner adapted to the specific requirements for missile defenses in different regions of the world. The administration is committed to building a European regional missile defense system, the European PAA or EPAA between now and 2020. The first elements of the EPAA were deployed in late 2011. However, much progress is still required in order to reach the goals set for the PAA. This article addresses the technological, operational and political issues confronting the Obama administration in its efforts to make the PAA a reality.     

基于门限偶极子模型的四轮车变速度轨迹跟踪控制

针对利用李亚普诺夫函数控制律设计的轨迹跟踪控制器在跟踪初始误差较大和离散轨迹时,存在速度跳变问题和拐点处误差偏大的问题,设计了一种基于门限偶极子模型和趋向模型的变速度轨迹跟踪控制器。以四轮车的运动学模型为研究对象,在李亚普诺夫函数控制律的基础上,引入门限偶极子模型解决了初始误差较大速度跳变问题,同时引入纵向控制中的趋向模型,解决了不连续轨迹拐点处误差偏大的问题,使得跟踪轨迹更为光滑,进一步提高了跟踪精度。通过仿真结果对比分析,验证了改进控制器的有效性。     

基于强跟踪扩展Kalman滤波的X射线脉冲星导航定轨精度研究

为提高X射线脉冲星导航定轨精度,依据脉冲星导航原理,建立了X射线脉冲星自主导航系统的状态方程和观测方程,提出用强跟踪扩展Kalman滤波（Strong Tracking Extended Kalman Filter,STEKF）替代扩展Kalman滤波,并对3颗脉冲星卫星运行的位置和速度估计进行了仿真实验。仿真结果表明：STEKF具有使滤波器能够自适应地校正估计偏差并迅速跟踪状态变化的能力,有效地提高了卫星运动状态的估计精度和数值稳定性。     

Multi-objectives nonlinear structure optimization for actuator in trajectory correction fuze subject to high impact loadings

This paper presents an actuator used for the trajectory correction fuze, which is subject to high impact loadings during launch. A simulation method is carried out to obtain the peak-peak stress value of each component, from which the ball bearings are possible failures according to the results. Subsequently, three schemes against impact loadings, full-element deep groove ball bearing and integrated raceway, needle roller thrust bearing assembly, and gaskets are utilized for redesigning the actuator to effectively reduce the bearings' stress. However, multi-objectives optimization still needs to be conducted for the gaskets to decrease the stress value further to the yield stress. Four gasket's structure parameters and three bearings' peak-peak stress are served as the four optimization variables and three objectives, respectively. Optimized Latin hypercube design is used for generating sample points, and Kriging model selected according to estimation result can establish the relationship between the variables and objec-tives, representing the simulation which is time-consuming. Accordingly, two optimization algorithms work out the Pareto solutions, from which the best solutions are selected, and verified by the simulation to determine the gaskets optimized structure parameters. It can be concluded that the simulation and optimization method based on these components is effective and efficient.     

基于虚拟目标的反舰导弹的最优制导律研究

为了对抗敌方预警系统的跟踪、预测以及远程防空导弹的拦截,反舰导弹的飞行弹道应采用大空域变轨弹道。将弹目相对运动分解为俯仰和航向两个平面内的运动,考虑了制导过程中能量消耗最小以及末端角度要求,分别设计了两个平面内的最优制导律。利用该制导律可以引导反舰导弹向大空域内任何虚拟目标进行变轨机动,从而实现了各种各样的大空域变轨弹道。只要虚拟目标参数设置合适,反舰导弹的各项性能指标均能满足要求。弹道仿真表明了所设计的最优制导律的有效性。     

弹道修正弹系统效能灵敏度分析

灵敏度分析是武器系统效能分析中的一项重要内容,针对正交试验的不足,在分析了弹道修正弹系统效能的影响因素的基础上,建立了基于均匀设计的弹道修正弹系统效能的回归模型。通过对模型求导得到了命中概率对各参数的灵敏度表达式,并进行优化分析,得到了系统效能参数的最优组合以及最优区间,研究结果可作为弹道修正弹参数优化设计的依据。     

基于双目视觉定位技术的无人船航迹跟踪控制室内模型实验

水面无人系统的航向控制与航迹跟踪技术在研究开发阶段一般在室内环境进行调试与运行,该过程需要定位系统进行辅助.实船常用的定位技术难以在室内发挥作用,现有的几种室内定位技术存在成本高、信号传播不稳定等问题.设计了一种基于双目视觉定位技术的船模航迹跟踪控制系统.结合实验场地和实验对象,通过在船模上布置特征物、图像预处理、图像...     

攻防对抗中弹道仿真的设计与实现

在攻防对抗仿真试验中,为了验证导弹性能、分析导弹战术指标,需要进行导弹群复杂环境下的弹道仿真试验,这给仿真实现带来了一定的困难。针对这一困难,在详细分析了六自由度下的弹道仿真的复杂情况的基础上,利用分布式计算的原理和标准,探讨了分布式仿真在导弹群复杂环境下弹道仿真中的应用方法及实现途径。