武器装备排气系统红外抑制器技术综述

主要介绍了排气系统红外抑制器的原理,归纳了建立抑制器模型的方法,列举了多种提高红外抑制器性能的方案和一些重要实验结果。同时对抑制器发展现状进行了介绍和总结,并作出了比较和展望。     

一种基于当前统计模型的模糊交互多模型算法

研究了模糊交互多模型算法(FIMM)和基于当前统计模型(CS)的自适应滤波算法,提出了一种基于当前统计模型的模糊交互多模型算法(CSFIMM)。该算法克服了模糊交互多模型算法精度较低和当前统计模型自适应滤波器方差调整有限的缺点。通过仿真,对所提出的算法和交互多模型(IMM)算法以及FIMM算法在估计精度和计算量两个方面进行了比较。     

一种运用遗传算法确定船舶航向控制模糊规则的方法

为了克服船舶航向控制模糊规则确定过程中的盲目性,引入一种与之相适应的遗传算法,以使结果成为某种意义下的最优解,从而从根本上解决这一重要问题.文中运用Matlab的C语言MEX-文件技术,将遗传算法源代码与Matlab直接结合起来,利用后者的强大建模能力,建立起完整的仿真模型.仿真结果表明,船舶的航向控制能力得到明显改善.     

模糊-专家控制在智能消磁中的应用研究

综合消磁是处理舰船固定磁性的重要手段.长期以来,由于综合消磁工艺的复杂性,使得这项工作在很大程度上依赖人工.实现消磁自动化,就是要将工作人员从繁重的脑体劳动中解放出来,提高工作效率.目前的新型消磁站已经实现了数据采集、统计自动化,不仅基本免除了工作人员的体力劳动,也从一定程度上减轻了消磁技师的脑力劳动.然而由于需要人工参与决策,综合消磁的效果和效率仍然十分依赖于人的因素.所以,实现综合消磁工作的完全自动化,补偿电流值组合的智能化决策是关键问题.本文在分析以前所做工作的基础上,运用模糊控制理论构造模糊-专家控制器,替代人工决策过程以实现自动化消磁.     

模糊偏序关系的一种信息集成方法

以模糊超过关系、模糊不协调关系为例,就模糊偏序关系给出了一种基于分组加权极大(极小)算子的信息集成方法,讨论了该方法的一致性、非独裁性等性质.     

月球轨道超长波天文观测微卫星在轨数据预处理方法

围绕“嫦娥4号”月球轨道超长波天文观测微卫星展开研究,针对微纳卫星对地数传资源的限制,提出一种在轨信号预处理方法：通过10通道数字下变频链路实现原始数据的变频接收,再利用多级滤波器抽取获得低采样率基带数据,下变频本振频率可调,在对地数传资源约束下保证了不同频带数据的灵活选取。以上方法实现了一种10频点超窄带梳状滤波,仿真验证表明,采样率80 MSPS基带带宽为1 kHz的情况下,此方法可在现场可编程门阵列平台上稳定运行,能保证带内平坦度和线性相位等关键技术指标, 数据量与直接下传原始数据相比,降低了3个数量级以上。     

Merely ‘Docile Self-Deception’? German Experiences with Nuclear Consultation in NATO

ABSTRACT

Recent nuclear-weapons-related consultation in NATO within the framework of the Defence and Deterrence Posture Review sheds light on historical experiences with nuclear consultation in NATO. In the early years of the Nuclear Planning Group (NPG), which became the main forum for multilateral nuclear consultation in the alliance, developing a nuclear weapons first use doctrine was of particular importance. This process led to the adoption of the Provisional Political Guidelines (PPGs) on the threat to initiate the use of nuclear weapons. With a focus on West Germany as the primary addressee of the NPG, it will be postulated that nuclear consultation functioned and may still be seen as an essential tool to manage the credibility of US extended nuclear deterrence in the framework of NATO.     

The fateful phoenix: the revival of Al-Qa’ida in Iraq

Although the Islamic State in Iraq and al-Sham (ISIS) is seen as a novel manifestation of Islamic extremism, it is in fact the latest, albeit perhaps the most effective, of a long line of revivalist movements in the Islamic and the Arab worlds. Its motivations – hisba and jihad – differ little from its predecessors and its ambitions – to create a state organised in accordance with the precepts of the Islamic caliphate – reflect a long-standing Islamic ambition. It differs, of course, in terms of the sophistication of its political and military strategies, which mirror the contemporary complexities of the world in which it operates, but its objectives recall long-standing Islamic ideals, even if articulated in radically brutal and extremist ways. More importantly, perhaps, ISIS or Da’ish, to give it its Arabic sobriquet, reflects the enormous degree of resentment inside the Middle East at the ways in which Western powers have intervened in regional affairs over recent years, particularly their support for regimes and economic systems there that have betrayed, in the popular imaginary, the essential principles of social justice that lie at the root of Islamic vision of ideal social order. Indeed, in many respects, its analysis of the world in which it operates and of the objectives it seeks differ little in essence from those any other resistance and rejectionist movement, whether religious or sectarian. More specifically, it has been the sectarian conflict that resulted from the reversal of political order in Iraq as a result of the 2003 American-led invasion that has driven the success of the movement in capturing widespread Sunni support. Whether it can manage the complexities of the administration of a state remains open to question.     

动态滑翔运动建模、机理分析与航迹优化

信天翁凭借动态滑翔的飞行技巧从梯度风中获取能量,从而在几乎不拍翅膀的情况下进行长时间、长距离飞行,这种技巧应用于小型无人机上可拓展其完成任务的能力。基于飞行器动力学对梯度风场中的无人机运动方程进行推导和简化处理;利用简化的运动方程,分别从非惯性参考系中的动能定理和机械能变化的角度,对动态滑翔获取能量的机理进行分析;利用微分平坦法,以最小平均控制输入变化率为目标函数,对徘徊模式和平移模式的动态滑翔航迹进行优化计算。分析结果表明:逆风爬升、顺风下滑是动态滑翔基本获能方式。优化结果表明:控制输入变得更加平滑,甚至出现阶段性的常值,使得控制更加简化;徘徊模式下,当风梯度作为决策变量时,优化过程可在[0,0.5 s-1]的区间上找到使得目标函数值最小的风梯度;平移模式下,目标函数值在该区间上单调递减。     

高轨双星辐射源跟踪的高斯和-容积Kalman滤波算法

针对辐射源运动方程和观测方程的强非线性,提出基于高斯和框架与5阶容积Kalman滤波(5CKF)的跟踪算法GS-5CKF。该方法将起始时刻的时差观测量所确定的位于地球表面的时差线按经度等间隔划分,初始化多个并行的5CKF,线性组合各滤波器的输出获得辐射源运动状态的估计。针对5CKF,提出新的非线性测度并引入滤波器分裂与合并,从而提高了跟踪精度,同时保持GS-5CKF算法复杂度基本不变。仿真表明,相对仅使用单个5CKF和基于高斯和框架但使用3阶容积Kalman滤波器的GS-3CKF等方法,提出的算法具有更高的估计精度。