Micro VAX—Ⅱ计算机专用实时接口设备

在实时数字仿真系统中,实时接口设备是仿真机和控制系统实物间的界面,它的性能直接影响着实时数字仿真的精度。本文简要介绍了专为MicroVAX—Ⅱ计算机研制的DSI-4型专用实时接口设备的构成、各功能板的设计,以及DSI-4专用实时接口的工作过程和使用方法。应该指出的是:只要改变连接计算机的总线接口板,DSI-4专用实时接口还可以方便地与其它计算机(例如,CompaQ386机)组成实时数字仿真系统。     

红外寻的精确制导系统红外干扰与抗干扰的仿真及其评估方法的探讨

对精确制导系统，现在不仅要考虑本身的系统干扰和随机干扰对系统制导精度的影响问题，更重要的是研究在复杂的红外干扰环境下的制导精度。不同的红外干扰环境的仿真方法，红外抗干扰的仿真试验及抗干扰效率的评估方法，在本文中作了研究。     

计测仪器与模拟仿真技术

综述了计测仪器的技术特点、计测仪器与模拟仿真技术及其发展趋势。     

仿真模型检验的新工具

本文是从阐述姿控系统仿真模型检测的重要性以及检测手段需不断改进的观点出发,介绍计算机频率特性测试软件(ftsp)的主要优点和用途。     

Changing law of launching pitching angular velocity of rotating missile

In order to provide accurate launching pitching angular velocity（LPAV） for the exterior trajectory optimization design, multi-flexible body dynamics（MFBD） technology is presented to study the changing law of LPAV of the rotating missile based on spiral guideway. An MFBD virtual prototype model of the rotating missile launching system is built using multi-body dynamics modeling technology based on the built flexible body models of key components and the special force model.The built model is verified with the frequency spectrum analysis. With the flexible body contact theory and nonlinear theory of MFBD technology, the research is conducted on the influence of a series of factors on LPAV, such as launching angle change, clearance between launching canister and missile,thrust change, thrust eccentricity and mass eccentricity, etc. Through this research, some useful values of the key design parameters which are difficult to be measured in physical tests are obtained. Finally,a simplified mathematical model of the changing law of LPAV is presented through fitting virtual test results using the linear regression method and verified by physical flight tests. The research results have important significance for the exterior trajectory optimization design.     

飞机维修训练成本的系统动力学分析

以飞机维修训练成本为研究对象,首先分析了成本产生的因果关系;然后绘制存量流量图,建立存量、流量、辅助变量、常量之间的关联方程并确定其初始值;在确定模型合理的基础上,分析模型的计算结果。分析结果表明本仿真方法具有一定的实用性。     

Drag coefficient modeling for grace using Direct Simulation Monte Carlo

Drag coefficient is a major source of uncertainty in predicting the orbit of a satellite in low Earth orbit (LEO). Computational methods like the Test Particle Monte Carlo (TPMC) and Direct Simulation Monte Carlo (DSMC) are important tools in accurately computing physical drag coefficients. However, the methods are computationally expensive and cannot be employed real time. Therefore, modeling of the physical drag coefficient is required. This work presents a technique of developing parameterized drag coefficients models using the DSMC method. The technique is validated by developing a model for the Gravity Recovery and Climate Experiment (GRACE) satellite. Results show that drag coefficients computed using the developed model for GRACE agree to within 1% with those computed using DSMC.     

基于粒子滤波的红外弱小多运动目标检测

针对低信噪比条件下红外图像序列中的多个弱小运动目标检测问题,提出了一种基于粒子滤波的多目标检测前跟踪方法.首先分析了红外图像的状态及观测模型,然后将弱小运动目标的检测转化为贝叶斯滤波框架下的检测前跟踪,并利用多个粒子滤波器予以实现.为了评估该算法的有效性,采用人工合成的红外图像序列对其进行测试,结果说明该算法可同时处理低信噪比条件下的多个弱小运动目标,检测和跟踪性能良好.     

金属基复合材料界面与内聚力模型的研究进展

首先对金属基复合材料的界面物相组成和检测、结合强度等方面的研究进展进行综述,基于传统断裂力学,对现有金属基复合材料界面相进行表征的内聚力模型进行分析,探讨了内聚力本构关系及参数获取方法,并对模拟仿真在金属基复合材料界面相中的应用进行了总结,提出了未来研究的重点和方向。     

自适应1553B总线通信功能系统级测试方法设计

一些通信卫星通过自适应1553B总线通讯,因此总线控制端在上电前对终端设备的内部遥测参数容量、存储位置是未知的,而是在系统上电后及运行期间动态地维护当前所有终端设备的状态信息,并由总线控制端通过对终端设备的轮询确定终端设备的总线接入状态,并动态获取终端设备的自描述信息,从而解决综合电子总线自适应性能单一、普适性差、数据动态交互机制弱的缺陷。针对某通信卫星自适应1553B总线通信功能,提出一种精准快捷的通信卫星1553B总线测试系统,通过1553B总线终端监视与处理设备,分别对1553B总线的自描述信息动态轮询获取功能和A/B总线自适应轮询功能进行测试,实现对自适应1553B总线实时监视与分析功能。实验表明,该测试系统有效验证了卫星1553B总线自适应通信功能,为总线通信的有效性和实时性提供保障。