基于分布式组网雷达的弹道目标三维进动特征提取

弹道目标微动特征提取是当前研究的一个热点,但在单基雷达中,由于视角限制,仅能提取目标在雷达视线方向上的微动分量,难以获得目标的真实三维微动参数.本文基于分布式组网雷达,利用组网雷达的多视角特性,提出了有翼弹道目标三维进动特征提取方法.首先基于目标锥顶散射点的微多普勒特征参数实现了目标空间三维锥旋矢量的重构,在此基础上,通过分析锥底边缘散射点的进动特征与微多普勒曲线的关系,提取了目标的进动周期、自旋周期、进动角、锥底半径、自旋轴与锥旋轴的交点位置等特征,并实现了目标长度的估计.仿真实验验证了算法的有效性,并进一步利用仿真实验分析了算法的鲁棒性.     

近炸引信终点弹道多普勒信号仿真平台

目前引信终点弹道回波信号仿真,一般使用各自开发的执行程序,这些方法不通用、计算有误差。为此,论文 建立了基于通用CAD 电磁散射模型和引信终点弹道回波模型的引信终点弹道多普勒信号仿真平台。平台基于CAD 软件 对目标进行建模,具有计算电磁散射特性和引信回波信号的功能,以及可视化输入功能。平台算法主要采用物理光学法、 物理绕射理论、等效边缘电磁流（EEC）法,同时考虑复杂目标的遮挡和局部照射问题。平台可以仿真各类引信、目标 和交会条件的多普勒回波信号。平台的算例结果与实测数据进行了对比,结果非常吻合。算例表明,软件平台可靠有效, 能为近炸引信设计提供依据和途径,具有较好的实用性、通用性。     

彩色图像中射流轨迹提取算法的研究

提出了一种基于RGB三色差的彩色图像中消防水炮射流轨迹的提取算法。首先在已知射流起点情况下向四周进行24个方向的扫描,确定射流的方向为米字形的8个方向之一,然后在此方向上执行双线扫描探测,直到满足某一阈值条件或到达图像的边界。实验结果表明,该算法在复杂背景下能准确完整地提取消防炮射流轨迹,算法的适应性较强。     

基于结构相似度的轨迹聚类算法

针对目前轨迹数据聚类直接以整条轨迹数据作为基本单元,导致聚类效果降低的问题,提出了基于结构相似度的轨迹聚类算法。算法引入轨迹结构的概念,并给出结构相似度计算函数来分析轨迹内外部特征。首先根据转角将轨迹划分成若干轨迹段,然后通过计算轨迹段的结构相似度来判断轨迹的匹配程度,进而完成轨迹聚类。真实数据的实验结果表明:该算法较其他同类算法分析轨迹更全面、效率更高;可以通过不同参数灵活调整特征的敏感度,聚类结果更具有实际意义。     

Stereodynamics in reaction O（1D） ＋ CH4 〉OH ＋ CH3

A theoretical study of the stereodynamics for reaction O(1D) + CH4→OH + CH3 has been carried out using the quasiclassical trajectory method(QCT) on a potential energy surface structured by Gonzalez et al. The integral cross sections(ICSs), differential cross sections(DCSs) and product rotational angular momentum polarization have been calculated. With the collision energy increasing, the ICS decreases. There is no threshold energy, because no barrier is found on the minimum energy path. The DCS results show that the backward and forward scatterings exist at the same time. With the collision energy increasing, the dominant rotation of the product changes from the right-handed direction to the left-handed direction in planes parallel to the scattering plane. In the isotopic effect study, the decrease of the mass factor weakens the polarization degree of the rotational angular momentum vectors of the products.     

Theoretical study of stereodynamics for the N+H2/D2/T2 reactions

The effects of isotopic variants on stereodynamic properties for the title reactions have been investigated using a quasi-classical trajectory method based on the first excited state NH2（I^2A＇） potential energy surface [Li Y Q and Varandas A J C 2010 J. Phys. Chem. A 114 9644]. The forward–backward symmetry scattering of the differential cross section can be observed, which demonstrates that all these reactions follow the insertion mechanism. Three angle distribution functions P（θr）, P（φr）, and P（θr, φr） with different collision energies and target molecules H2/D2/T2 are calculated. It is shown that the product rotational angular momentum is not only aligned, but also oriented along the direction perpendicular to the scattering plane. The title reaction is mainly governed by the ＂in-plane＂ mechanism through the calculated distribution function P（θr, φr）. The observable influences on the rotational polarization of the product by the isotopic substitution of H/D/T can be demonstrated.     

Fuel-optimal trajectory design using solar electric propulsion under power constraints and performance degradation

The fuel-optimal transfer trajectories using solar electric propulsion are designed considering the power constraints and solar array performance degradation.Three different performance degradation models including linear,positive and negative exponential degradations are used in the analysis of three typical rendezvous missions including Apophis,Venus and Ceres,respectively.The optimal control problem is formulated using the calculus of variations and Pontryagin’s maximum principle,which leads to a bang-bang control that is solved by indirect method combined with a homotopic technique.In demonstrating the effects of the power constraints and solar array performance degradation on the power budget and fuel consumption,the time histories of the power profile and the fuel consumptions are compared for the three missions.This study indicates that it is necessary to consider the power constraints and solar array performance degradation for the SEP-based low-thrust trajectory design,espacially for long-duration outbound flights.     

碰撞能对反应Sr+CH_3I→SrI+CH_3的立体动力学影响

采用准经典轨线方法,基于半经验的London-Eyring-Polanyi-Sato势能面,研究了碰撞能对碰撞反应Sr+CH3I→SrI+CH3的立体动力学性质的影响.结果表明,反应物的初始碰撞能对产物转动角动量矢量的取向和定向程度都有重大影响.     

转动激发对H+LiF→HF+Li的立体动力学影响的理论研究

用准经典轨线方法在Aguado-Paniagua2(AP2)势能面上计算了反应物转动量子态对H+LiF→HF+Li反应立体动力学的影响. 给出了关于产物和反应物之间矢量相关的P(μr)和P(ár)的分布情况. 同时计算了四个极化微分反应截面. 结果表明转动量子态对H+LiF→HF+Li反应的矢量性质有很大影响. 还计算了H+LiF→HF+Li反应的反应几率.