基于轨迹线性化方法的导弹动态逆控制系统设计

基于动态逆控制及轨迹线性化方法,研究了一种新的导弹鲁棒自适应控制系统设计方法.首先,基于导弹的非线性模型设计快、较慢回路的动态逆控制器,以实现其非线性解耦;然后,在较慢回路中设计鲁棒自适应轨迹线性化控制器,以补偿整个控制系统的不确定性及干扰,即在轨迹线性化控制的基础上,通过设计RBF神经网络在线估计系统中存在的不确定性...     

菲利普斯曲线之中国验证——基于1985-2004年的数据分析

本文在介绍分析菲利普斯曲线三种形态及其政策含义的基础上,使用中国的相关数据对其进行验证。本文对我国菲利普斯曲线的三种形态分别进行绘制和分析。在简要回顾对曲线走势有重要影响的宏观经济政策之后,提出当前应当逐渐由扩张性财政政策向中性的财政政策转变。     

一类中立型高维周期微分系统的周期解

文中利用指数型二分法,结合不动点定理考虑如下形式的中立型高维周期系统: 苦d/dt[x(t)+cx1]=A(t,x(t))x(t)+f(t,x1),得到其T-周期解存在的充分性条件,所得结论改进或推广了早先文献中周期解存在的相应结论。     

基于Kohonen自组织网络算法规划数控抛光路径

为避免在数控抛光中因采用规则运动路径产生的规律性高频误差,故借助于神经网络方法,采用基于Kohonen自组织网络算法,对抛光头的运动路径进行规划。     

一步法制备BAMO-THF型热塑性弹性体及其力学特性

以一缩二乙二醇(DEG)为扩链剂,通过一步熔融聚合法,制备得到高含量3,3-二叠氮甲基氧丁环与四氢呋喃共聚醚(BAMO-THF)型含能热塑性弹性体(ETPE)。采用傅里叶变换红外光谱(FT-IR)和广角X-射线衍射仪(WXRD)表征制备的ETPE结构,动态力学热分析(DMA)、万能材料试验机、邵氏硬度仪研究其力学性质。结果表明,制备的BAMO-THF型ETPE具有明显的叠氮型聚醚聚氨酯弹性体特征。在加载应力和温度作用下,由于其线性分子链结构,ETPE试样蠕变程度较大。此外,扩链剂含量的增加并不利于ETPE延伸率和低温性能的提高。其中软段BAMO-THF含量达到93.3%,硬段含量仅为6.7%的D20试样力学性能较佳,抗拉强度和断裂伸长率分别为3.61 MPa和1 277%,低温玻璃化转变温度为-23.4℃。     

Energetic neutral atom (ENA) and charged particle periodicities in Saturn’s magnetosphere

The Magnetospheric Imaging Instrument (MIMI) on the Cassini spacecraft has observed energetic neutral atoms (ENA) and charged particles at Saturn from mid-2004 to the present. The particles often but not always reveal striking periodic behavior that seems to depend on the type of particle and spacecraft location. When subjected to a Lomb periodogram analysis, energetic electrons (>150 keV) exhibited strong frequency peaks near 10.80 h (the nominal or “base” period of Saturn kilometric radiation) during 2006–2008, but essentially no periodicity during 2005. The electron periodograms also show pronounced “double” frequency peaks in 2007 and 2008. Energetic protons (3–26 keV) show strong peaks near the same period for 2005–2007, but none for 2008. Oxygen ions at the same energies display strong peaks for 2005 and 2006, but not for 2007 and 2008. By projecting the ENA images onto Saturn’s equatorial plane or onto a plane perpendicular to the equatorial plane and then summing the data in the appropriate dimension, “strip” images can be constructed from which a time history can be derived. These time histories of ENA emissions are also subjected to a Lomb periodogram analyses. The energetic hydrogen neutrals (20–50 keV) exhibited periodic behavior only during 2007, while energetic oxygen neutrals (64–144 keV) displayed a strong SKR-like period in 2005 and 2006 but not for 2007 or 2008. Some of this behavior may be due to changing spacecraft aspect relative to the ENA emissions, and some of it may be real. This periodic behavior may be consistent with a rotating anomaly that “flashes” brightly in the midnight-to-dawn sector once per 10.8 h, with the flash parameters depending on particle species and energy.     

近月空间带电粒子环境——“嫦娥1号”“嫦娥2号”观测结果

“嫦娥1号”（CE-1）、“嫦娥2号”（CE-2）都安装了1台太阳高能粒子探测器（High-energetic ParticlesDetectors,HPD）和2台太阳风离子探测器（Solar Wind Ion Detectors,SWIDs）,进行了月球轨道200 km和100 km空间环境探测,获得了月球轨道空间高能带电粒子（质子、电子和重离子）能谱随时间的演化特征、等离子体与月球相互作用特征以及太阳风离子速度、密度和温度参量。空间环境探测数据分析结果表明：太阳活动低年、空间环境扰动水平相对较低、月球处于太阳风中时,近月空间带电粒子环境的基本特征与行星际空间相比变化不大。CE-1、CE-2在轨运行期间,发现了多起0.1～2 MeV能量电子急剧增加事件,这些事件发生在月球从太阳风运动到磁尾的所有空间区域,其中20%的事件伴随着卫星周围等离子体离子加速。模拟和统计研究表明：能量电子急剧增加使得绕月卫星和月球表面电位大幅下降导致了离子加速现象的发生;能量电子总流量大于10¹¹ cm^-2时,绕月卫星和月球表面充电电位可达负的上千伏。此外,月表溅射与反射太阳风离子、太阳风“拾起”离子等空间环境事件的发现,揭示了太阳风离子和月球存在复杂的相互作用过程。     

对称负重合型气动伺服阀零位流动状态分析

针对负重合型气动伺服阀(PSV)零位特性设计缺少理论依据问题,根据单个节流口的气体质量流量公式建立起气动伺服阀滑阀级的数学模型,采用假设求证法分析了零位时气体流经上、下游节流口的流动状态与影响因素之间的关系。结果表明在不同供、排气压力比下,负重合量不均等系数小于0.5283的气动伺服阀有3种可能的零位流动状态,即上、下游节流口均为亚声速流动,或者均为声速流动,或者上游节流口为声速时下游节流口为亚声速流动;负重合量不均等系数不小于0.5283的气动伺服阀有两种可能的零位流动状态,即上、下游节流口均为亚声速流动,以及上游节流口为亚声速时下游节流口为声速流动。可知气动伺服阀的零位流动状态由负重合量不均等系数与供、排气压力比共同决定。以负重合量不均等系数分别为0.5、1、2的气动伺服阀为例进行了计算和实验验证,实验结果与理论分析相吻合。     

Solar proton events recorded in the stratosphere during cosmic ray balloon observations in 1957–2008

Long-term balloon observations have been performed by the Lebedev Physical Institute since 1957 up to the present time. The observations are taken several times a week at the polar and mid latitudes and allow us to study dynamics of galactic and solar cosmic ray as well as secondary particle fluxes in the atmosphere and in the near-Earth space. Solar energetic particles (120) – mostly protons – (SEP) events with >100 MeV proton intensity above 1 cm⁻² s⁻¹ s⁻¹ were recorded during 1958–2006. Before the advent of the SEP monitoring on spacecraft these results constituted the only homogeneous series of >100 MeV SEP events. The SEP intensities and energy spectra inferred from the Lebedev Physical Institute observations are consistent with the results taken in the adjacent energy intervals by the spacecraft and neutron monitors. Joint consideration of the SEP events series recorded by balloons and by neutron monitors during solar cycles 20–23 makes it possible to restore the probable number of events in solar cycle 19, which was not properly covered by observations. Some correlation was found between duration of SEP event production in a solar cycle and sunspot cycle characteristics.     

中性稳定的舰载飞机着舰模态研究

由于舰载飞机着舰前处于跟踪雷达的盲区，此时导引系统关闭，为了使飞机的姿态及轨迹角在舰尾气流扰动下力求不变，以达到安全着舰的目的，提出了飞机中性稳定的新型着舰模态，其实现途径是利用后缘襟翼对称偏转所产生的直接力，对迎角小扰动变化进行气动解耦，从而构成中性稳定舰载飞机，使飞机动力学的特征模态由振荡型转变为非周期型。仿真结果表明，该模态可有效地抑制气流扰动，提高着舰的安全性。