通用飞行动力学模型库的开发及应用

飞行动力学模型是飞行仿真技术的基础,以往动力学模型的研究集中在数值解算方法上,忽略了模型本身的重用性、互操作性问题。采用面向对象方法构建飞行动力学模型框架,使用XML语言将飞行器各种特性数据组织起来,开发了一个通用的飞行动力学模型库,并实现了与飞控系统模型的一体化设计与开发。     

有输入未建模动态和不确定性导弹控制器设计

在考虑导弹控制系统同时存在输入未建模动态和参数不确定性的情况下,提出了一种基于RBF神经网络和反演技术的鲁棒自适应控制器的设计方法。首先用两个RBF神经网络对未建模动态进行了补偿,然后利用反演技术设计了鲁棒自适应控制器,对不确定性进行了处理,并用Lyapunov稳定性理论推导出RBF神经网络的权重矩阵调节率以及相关的自适应律,证明了系统的全局稳定性,最后通过仿真计算验证了设计的正确性。     

Coronal Dynamics and the AIA on SDO

We provide a brief overview of present-day studies of inner corona dynamics, with examples of mass ejections (CME), flares and active region dynamics. While the names of the topics have not changed in several decades, the internal details and the language used to express the nature of the problem have changed considerably. We conclude with a short discussion of the contribution to studies of coronal dynamics to be expected from the Atmospheric Imager Assembly (AIA) on the Solar Dynamics Observatory.     

Self-consistent amplitude profile of ducted VLF transmitter signal due to resonant interaction with energetic electrons in the magnetosphere

Of the various sources of whistler waves in the magnetosphere, the signals from terrestrial VLF transmitters are apparently the simplest for theoretical analysis. The role of these signals in the acceleration and pitch-angle scattering of energetic electrons in the Earth’s radiation belts has not been fully studied quantitatively, despite many decades of relevant research. The main problem in studying this issue is that to calculate the acceleration and pitch-angle scattering of particles, it is necessary to know the spatial profile of the signal amplitude. This is especially critical for phase-trapped particles, for which the energy exchange with the wave is the most significant. At the same time, the wave amplitude profile itself is determined by the interaction of the wave with resonant particles. Thus, we are dealing with a self-consistent problem, which is described by a nonlinear system of equations - a kinetic equation for the distribution function of resonant particles with a self-consistent field, and an equation for the wave field, in which the nonlinear and non-local growth rate is determined by the distribution function of resonant particles. In this paper, we develop an approach to solving this system of equations and the corresponding physical problem using the method of successive approximations.     

Observational constraints on dark matter in the universe

Application of the cosmic virial theorem to galaxy redshift surveys suggests an open universe - if the dark material is distributed in the same way as galaxies. Here we investigate four redshift surveys. We present new results on the amplitudes of the two- and three-point galaxy correlation functions and we estimate the relative peculiar velocities in the deep redshift survey of Kirshner and co-workers (1983). Next, we review evidence which suggests that dark material is clustered on scales comparable to the optical radii of galaxies. In particular, we use spectroscopic and photometric observations to set constraints on the mass distribution in elliptical galaxies.     

固体火箭发动机真实流体输运系数的自动模拟

为缩短固体火箭发动机的研究周期、降低研究成本和揭示工作机理,需要对其工作过程进行三维数值仿真,但数值计算中许多物性参数如输运系数的确定存在困难,为此主要研究了适合于固体火箭发动机内高温高压下的多组分混合物输运系数的计算方法,并通过高级计算机语言管理数据库等方法实现自动计算,可准确快速地计算发动机内流过程中输运系数的变化,为真实模拟发动机的工作过程提供正确的物性参数。     

上风格式的若干性能分析

采用理论分析和数值试验相结合的方法，对上风格式的三个典型代表：FDS、FVS及AUSM格式的性能进行了分析比较：FDS格式具有高的间断分辨率但可能出现非物理懈；FVS格式捕捉强非线性波的能力很强，计算效率高，但耗散比较大；AUSM格式兼有高间断分辨率和高计算效率且克服了两者的弱点。以一维无粘激波管流场为算例考察了这些格式性能与间断分辨率。     

拖曳系统基本飞行性能算法研究

分别采用拖缆模型中的刚化柔性悬索和线性弹簧模型对拖曳系统的起飞性能和平飞性能进行了仿真计算。计算结果表明．运载器的质量和气动特性对拖曳系统的飞行性能影响极大，拖缆采用刚化柔性悬索和线性弹簧模型的计算结果基本一致．说明在拖曳系统中，上述两种拖缆模型的使用是适当的。     

E 级计算给 CFD 带来的机遇与挑战

E 级(Exascale)计算机有望在2020年前后投入使用,E 级计算将给计算科学和科学研究带来革命性的变化。计算流体力学(CFD)作为超大规模计算机应用的重要领域之一,将迎来前所未有的发展机遇,同时也将面临极其严峻的技术挑战。本文对当前国内外超大规模 CFD 计算的现状进行了概述,探讨了未来 CFD 的发展趋势,并对 E 级计算给 CFD 带来的机遇与挑战进行了分析,最后提出了适应未来 E 级计算的 CFD 发展思路与建议。为了实现 E 级计算的宏伟目标,CFD 与计算机科学、应用数学等学科的“协同设计”势在必行。我们期待本文的分析能对我国的高性能计算应用、CFD 发展有一定的启示作用。     

一种叶轮机三维叶型黏性反问题方法

提出了一种应用于叶轮机三维叶片气动设计的黏性反问题方法,该方法将叶片表面边界视为是运动的壁面,通过建立并求解壁面法向动量方程,从而可根据给定的压力分布或压力面与吸力面之间的压力差分布直接求解叶型几何.结果表明:该方法可与定常雷诺平均Navier-Stokes(RANS)模拟配合进行求解,鲁棒性强、计算耗时短,且符合真实黏性流动环境,无需对叶型进行黏性修正.算例验证结果显示,该方法在单排和多排叶片环境下都能获得反问题解,计算稳定性和收敛性良好.