一个基于面向对象模型的并行系统

为了开发分布式系统中的计算资源,我们设计了一个基于面向对象大粒度数据流模型的并行Ｃ＋＋系统ＯＯＣＰＣＳ．该系统的底层计算模型是面向对象范式和数据流模型的结合体。它将状态对象引入到数据流模型中,并且支持面向对象的特性。本文讨论了此模型在ＯＯＣＰＣＳ系统中的实现;并行化编译器;ＰＯＣ程序设计语言;面向对象网络文件Ｉ／Ｏ和虚拟ＯＯＬＧＤＦＭ机     

角速率火控原理研究

论述并研究了角速率火控原理,利用“滤波──识别”方法,提出了一套新的角速率火控滤波和外推模型。仿真结果表明,这种模型对于机动运动的反舰导弹可以明显提高火控预报精度。     

紧固件用钢复验的动态抽验方案

本文针对现行紧固件原材料进厂抽样复验方法的不足,套改《ISO2859计数抽查程序和图表》,提出动态抽样方案,并对新旧方案实际应用进行了比较。以比较科学的决策,取得提高效益、降低消耗的结果.     

就业问题对边防部队思想政治工作的影响

军人就业问题对边防部队思想政治工作有很大的影响 ,必须努力创造良好的军人就业条件 ,打牢部队“打得赢 ,不变质”思想政治工作的基础。     

对加强农村消防工作的思考

针对我国农村消防工作现状 ,就如何加强农村消防工作谈几点看法 ,旨在全面提高农村整体防灾能力。     

通用导弹告警设备的试验和研究

导弹在进攻时,其截面相当于一个偶极子天线或单根箔条,利用导弹对特定频率雷达信号的谐振特性来增大目标的散射截面积。通过反辐射导弹告警实验设备系统的实弹打靶试验,验证了该理论的正确性和可行性。     

一种面向对象类级状态测试的形式化方法研究

面向对象的软件开发给测试带来了新的挑战,传统的测试技术不能直接用于面向对象的软件测试中,必须对其进行扩充和完善.类级测试是面向对象测试过程中的一个重要阶段,而类状态的测试是类级测试的核心.作者将扩充后的黑盒测试技术应用到类状态的测试过程中,可直接使用方法级的测试数据有效测试类中方法间的交互及其类状态的变化.最后,通过一个实例说明对类级状态的测试及其测试用例的生成.     

Supercritical carbon dioxide as a new working medium for pneumatic launch: A theoretical study

Compared with the conventionally gaseous or liquid working media, the specific internal energy of supercritical carbon dioxide (SCD) is higher at the same temperature and pressure, and the critical temperature of carbon dioxide is close to room temperature, making SCD a potential new working medium for pneumatic launch. To analyze the feasibility of this conception, an analytical model of a pneumatic catapult is established on basis of the conservations of mass and energy. The model consists of a high-pressure chamber and a low-pressure chamber connected by multiple valves, and there is a movable piston in the low-pressure chamber that can push an aircraft to accelerate. The effects of the launch readiness state of SCD in the high-pressure chamber, the initial volume of the low-pressure chamber and the valve control on the movement of the aircraft are analyzed. It is found that there is a restrictive relation between the temperature and pressure of the launch readiness state of SCD, i.e., there is a maximum allowable launch readiness pressure when the launch readiness temperature is fixed. If this restrictive relation is not satisfied, the working medium in the low-pressure chamber will drop to its triple point within a few milliseconds, leading to a launch failure. Owing to this restrictive relation, there is an optimal launch readiness state of SCD with the highest working capacity for any allowable launch readiness temperature. The pressure of the low-pressure chamber will decrease significantly as the initial volume increases, leading to a decreased acceleration of the aircraft. The ac-celeration can be controlled below a critical value by a designed sequential blasting technique of multiple valves. The calculated results show that a 500 kg aircraft can be accelerated from 0 to 58 m/s in 0.9 s with 36 kg of carbon dioxide. This research provides a new technique for the controllable cold launch of an aircraft.     

反作用轮低速特性观测补偿方法

反作用轮在现代高精度卫星姿态控制中占据着重要的地位。但由于反作用轮工作于低速状态,其转速过零时摩擦力矩的非线性特征将会对姿态控制精度产生较大的影响,并影响卫星运行寿命。基于Dahl摩擦模型建立了直流电机驱动的反作用轮系统数学模型,在此基础上设计了用于改善反作用轮低速性能的补偿观测器,并将其应用于三正交结构姿态控制系统。数字仿真说明此方法可以有效地抑制反作用轮低速摩擦产生的扰动,从而大幅度改善卫星姿态控制精度及其姿态稳定性。最后探讨了该观测器方法同变结构控制方法的综合应用前景。     

人性结构和规律与现代思想政治教育

现代思想政治教育以促进人的自由全面发展为根本目标。在思想政治教育实践活动中,必须把握人性结构,遵循人性发展变化的基本规律,关注人的属性满足规律,把握人性结构动态平衡规律,遵循精神境界提升规律,更加有效地完成现代思想政治教育任务和教育目标的有效结合,努力促进教育目标和教育手段的有效结合,实现人的全面发展。