航空武器项目区间DEA评价与决策

航空武器装备项目评价方法的科学性直接影响评价结果的准确性.在对DEA方法分析总结的基础之上,针对航空武器装备项目常用评价方法的局限性,以及航空武器装备项目规划评价阶段数据的不确定性,本文利用IDEA(区间数据包络分析)方法建立了航空武器装备项目方案有效性评价模型,并进行了实例研究.评价结果表明,本文所提出的IDEA评价决策方法不仅弥补了传统DEA方法的不足,而且克服了常用方法主观性强的弱点,因此其评价结果更加全面、更加符合实际情况.     

An experimental study of the dual-loop control of electro-hydraulic load simulator （EHLS）

This paper investigates motion coupling disturbance（the so called surplus torque）in the hardware-in-the-loop（HIL）experiments.The＇＇velocity synchronization scheme＇＇was proposed by Jiao for an electro-hydraulic load simulator（EHLS）in 2004.In some situations,however,the scheme is limited in the implementation for certain reasons,as is the case when the actuator＇s valve signal is not available or it is seriously polluted by noise.To solve these problems,a＇＇dual-loop scheme＇＇is developed for EHLS.The dual-loop scheme is a combination of a torque loop and a position synchronization loop.The role of the position synchronization loop is to decouple the motion disturbance caused by the actuator system.To verify the feasibility and effectiveness of the proposed scheme,extensive simulations are performed using AMESim.Then,the performance of the developed method is validated by experiments.     

Application of ADER Scheme in MHD Simulation

The Arbitrary accuracy Derivatives Riemann problem method(ADER) scheme is a new high order numerical scheme based on the concept of finite volume integration,and it is very easy to be extended up to any order of space and time accuracy by using a Taylor time expansion at the cell interface position.So far the approach has been applied successfully to flow mechanics problems.Our objective here is to carry out the extension of multidimensional ADER schemes to multidimensional MHD systems of conservation laws by calculating several MHD problems in one and two dimensions: (ⅰ) Brio-Wu shock tube problem,(ⅱ) Dai-Woodward shock tube problem,(ⅲ) Orszag-Tang MHD vortex problem.The numerical results prove that the ADER scheme possesses the ability to solve MHD problem,remains high order accuracy both in space and time,keeps precise in capturing the shock.Meanwhile,the compared tests show that the ADER scheme can restrain the oscillation and obtain the high order non-oscillatory result.     

用于气动声学计算的非均匀网格紧致差分格式

为克服传统紧致差分格式在数值求解非均匀网格问题时产生的寄生波,构造了一种新的高精度紧致差分格式.通过泰勒展开分析方法,详细给出了格式系数的通用形式;利用傅里叶分析方法,分析了数值耗散、色散误差.以3对角6阶精度紧致差分格式求解均匀扰动网格问题为例,计算表明:色散值和耗散值随扰动因子的增加而更加趋近于精确值;当扰动因子大于0.213时,格式不稳定,当扰动因子小于等于0.213时,格式渐近稳定;对一维对流波和二维波传播的模拟计算所得数值解与精确解吻合,体现了该格式在求解非均匀网格问题时的优越性.      

火星进入段自主导航技术研究现状与展望

基于国际上成功着陆的火星探测任务和未来火星着陆探测技术的发展需求,阐述了火星进入段自主导航的必要性。首先总结了火星进入段自主导航技术的研究现状与发展趋势,随后分析了火星进入段自主导航的特点以及所面临的挑战,并概括了火星进入段自主导航所涉及的关键技术。最后对我国未来火星探测任务进入段的自主导航技术发展方向进行了展望。     

台阶流模型流场的局部DQ-Lagrange求解方法

以Lagrange多项式作为Differential Quadrature(DQ)方法的基函数,应用局部DQ-Lagrange方法对Navier-Stokes方程进行了数值求解,建立了基于局部迎风DQ-Lagrange方法的复杂台阶流流场求解模型.并在此研究基础上,提出了本质和自然边界条件的处理方法.分析了支持域的选择、边界条件处理方法、迎风机制等对求解精度的影响.结果表明:支持域较大时,Lagrange高阶插值易出现振荡现象,可以采用局部替代全局的插值方法;迎风支持域的加入可以提高求解精度;建模时速度支持域的选择应该大于压力支持域.      

A numerical model characterizing internal gravity wave propagation into the upper atmosphere

A new two-dimensional, time-dependent and fully nonlinear model is developed to numerically simulate plane wave motions for internal gravity waves in a non-isothermal and windy atmosphere that accounts for the dissipation due to eddy and molecular processes. The atmosphere has been treated as a well mixed total gas with a constant mean molecular weight. The effects of Rayleigh friction and Newtonian cooling are applied near the upper boundary of the model to simulate the radiation conditions as well as to act as a sponge layer; lateral boundaries are periodic over a horizontal wavelength to simulate a horizontally infinite domain. The thermal excitation to initiate upward propagating waves is spatially localized in the troposphere and is a Gaussian function of time. A time-splitting technique is applied to the finite difference equations that are derived from the Navier–Stokes equations. The time integration for these highly coupled equations is performed using an explicit second order Lax–Wendroff scheme and an implicit Newton–Raphson scheme. The wave solutions derived from the model are found to be broadly agreeable with those derived from a Wentzel–Kramers–Brillouin theory.     

短消息公钥加密构造Tag-KEM方案

Tag—KEM／DEM是2005年提出的一种混合加密结构。Tag—KEM（Tag密钥封装机制）是其组成部分,采用公钥加密技术封装密钥。针对混合加密中不宜用慢的长消息公钥加密的问题,提出了一种用短消息公钥加密方案构造Tag—KEM方案的通用方法;结果证明了该方法在随机预言机模型下选择密文安全。该方法对Tag部分的处理不会带来额外的冗余,是第一个无需验证Tag部分有效方案。表明Tag—KEM／DEM结构优于KEM＋DEM。     

低耗散高可信度格式及其在气动力热计算中的应用

本文简要介绍了TVD类型格式中近似黎曼解的耗散机理,该耗散机制对于粘性问题的计算有较大的负面影响.通过引入低耗散的格式,所发展的数值方法对粘性流场的气动力热问题的计算具有较高的精度.以该数值方法为基础发展的软件系统,在亚跨超和高超声速领域中的气动力热问题上均得到了验证,计算结果与实验进行了对比验证,表明该计算软件系统具有较高的可信性.     

失效卫星再利用系统方案设想

为了实现在轨资源再利用,文章分析了失效卫星再利用的可能性,根据卫星不同的失效模式,包括入轨失败、部件失效、寿命末期,得出系统的4类轨道操作任务。论述系统的五大组成部分,并分析了各个系统间的关系;比较了货运飞船和搭载两种上行方案各自的优缺点;结合系统特点,在分析系统任务功能的基础上提炼出了6项相关关键技术。从系统角度提出了有利于失效卫星再利用系统可尽早实现的3条途径。