载荷分布对六自由度运动平台动力学性能的影响

用Newton-Euler方法,分析了运动平台的力矢和力矩,建立了统一的六自由度运动平台动力学方程。利用该方程研究了不同载荷分布时六自由度运动平台各液压缸的受力情况,并用Matlab进行了计算。结果表明,不同载荷分布时,某些液压缸的驱动力的最大值成倍增加,变化极为复杂,为六自由度运动平台的设计及控制提供了理论指导。     

A novel launch dynamics measurement system for multiple launch rocket system and comparative analysis with numerical simulations

In this paper,a novel launch dynamics measurement system based on the photoelectric sensor pair is built.The actual muzzle time(i.e.a time duration that originates from the initial movement to the rocket's departure from the muzzle)and the muzzle velocity are measured.Compared with the classical methods,the actual muzzle time is obtained by eliminating the ignition delay.The comparative analysis method is proposed with numerical simulations established by the transfer matrix method for multibody systems.The experiment results indicate that the proposed measurement system can effectively measure the actual muzzle time and reduce the error of classical methods,which match well with the simulation results showing the launch dynamics model is reliable and helpful for further analysis and design of the MLRS.     

系统动力学炮兵侦察感知系统能力生成建模与仿真

信息化作战,侦察感知能力是炮兵获取决策优势与行动优势的基础。依据炮兵侦察感知系统的功能与构成,分析炮兵侦察感知信息流程,运用系统动力学分析侦察感知系统的各要素及影响关系,进而建立炮兵侦察感知系统作战能力生成的系统动力学模型。依据设定作战背景,仿真分析了传感器性能、网络性能等对炮兵侦察感知系统能力生成影响问题,得出了较为可靠的结论,为炮兵基于信息系统体系作战能力要素建设提供决策依据。     

航天器推进系统模块化建模方法

为了研究由复杂增压气路和推进剂供应管路组成的航天器推进系统的动力学问题,基于AMESim软件平台,构建了模块化、可扩展的航天器推进系统仿真模型UPSSim.模型中,增压气路采用分段集中参数模型,推进剂供应管路采用分布参数模型,并考虑了系统各组件与环境的换热.对某型轨控发动机的变轨过程进行了仿真,UPSSim能准确模拟该发动机变轨过程中系统参数的变化,计算结果与设计性能参数、飞行遥测数据吻合较好.仿真结果表明,本文所采用的模块化建模与仿真方法适用于复杂管网的建模,在航天器推进系统仿真建模与仿真领域具有较好的应用前景.     

论三个代表的人本观

主要从党的宗旨、党的执政过程和执政目的、党的性质三个方面论述“三个代表”重要思想中所包含的中国共产党“以人为本”的执政理念     

At war with social theory: Instrumental and communicative action in US military doctrine during the War on Terror

As US counterinsurgency campaigns draw to a close, doctrine for asymmetric warfare written during the War on Terror has come under heavy criticism. While many have argued that this shift to ‘winning hearts and minds’ is evidence that the United States is taking humanitarianism and nation-building seriously, others argue that a wide gap exists between US counterinsurgency doctrine and the protection of civilians afflicted by conflict. In this article, I show that the latter is true by comparing theories of instrumental and communicative action to US doctrine for operational design, stability operations, and counterinsurgency. I argue that these texts treat the people as an object to be manipulated for the achievement of pre-determined self-interested strategic goals rather than members of a community that jointly designs operations to fulfill shared objectives. However, US doctrine does contain communicative elements that, if prioritized, would better support humanitarian and state-building objectives otherwise subordinated in the War on Terror.     

一种简化的弹道方程模型研究

弹丸在飞行过程中受到空气动力的作用,空气动力的系数也难以确定,这造成弹丸运动方程非常复杂.从空气动力对弹丸的作用效果出发来分析空气动力的变化,然后根据弹丸在飞行过程中受到的空气动力提出了一种简化的弹道方程模型,并通过对某射表的分析计算验证其有效性.     

大型商业性建筑安全疏散策略研究

近年来,大型商业性建筑火灾事故时有发生,造成了重大损失,火灾发生时如何提高人员的疏散效率是降低伤亡率的要素.通过对大型商业性建筑火灾危险性和疏散中存在的问题进行分析,结合实际从设置消防救援窗,严格划分防火分区,合理设置疏散楼梯和安全出口,制定安全疏散预案,加强消防安全培训,充分利用声光报警等方面论述了优化大型商业性建筑人员疏散效率的策略.     

Madagascar

Despite a constitution that condemns discrimination, as well as positive efforts by all stakeholders, Madagascar is still far from meeting the desired objectives of the Southern African Development Community (SADC) Protocol on Gender and Development, or any other relevant international instruments and conventions. The establishment of an Organising Technical Committee on security sector reform for Madagascar is a positive development, which will hopefully facilitate an understanding of the multiple facets of gender and security in Madagascar as well as advancing the implementation of the instruments calling for greater female participation in the security sector.     

超空泡航行体刚柔耦合动力响应有限元分析

考虑航行体大范围转动,根据哈密顿原理推导了超空泡航行体在一次近似模型变形下的刚柔耦合动力响应方程,定性分析了其与零次近似模型下方程的区别,并对方程进行了定量计算。结果表明:一次近似模型相比零次近似模型下的横向振动方程,刚度矩阵项增大;所推导方程能够用于定量分析和直观描述超空泡航行体刚柔耦合下的变形。