消防法中责令停止执业的法律依据

《消防法》规定的责令停止执业是对有法定消防行政违法行为的单位予以暂停相应资质、资格的一种处罚措施。其处罚主体为国家认证认可监督管理委员会以及地方质检部门;其处罚过程应适用听证程序,并确认、核实情节是否严重;其处罚实施应附有合理期限,同时需要采取相应保障措施。     

国际海洋法与维护国家海洋权益

海洋权益是指沿海国对属于自己的管辖海域享有国际海洋法所赋予的特定主权权利。《联合国海洋法公约》奠定了现代国际海洋法制度的基础，为各国维护正当的海洋权益提供了基本法律依据，但也有不完善甚至严重缺陷之处。认真研究其利弊，以切实维护国家海洋权益和公正合理的国际海洋法律秩序。     

高超声速滑翔飞行器变轨段自适应跟踪制导方法

针对高超声速滑翔飞行器变轨段大偏差条件下的标准轨迹跟踪问题,提出一种基于权值矩阵自适应修正的变轨段跟踪制导方法。分析了变轨段主要控制方式和标准轨迹特性;将简化的纵向运动方程在标准轨迹附近线性化;采用将误差项引进线性二次型性能指标加权矩阵的方式,设计了改进的权值自适应修正跟踪制导方法。CAV-H飞行器仿真分析表明,该方法能够实现高超声速滑翔飞行器变轨段高精度自适应跟踪制导,对初始及过程偏差具有良好的鲁棒性。     

论武警法学的建构

中国人民武装警察部队是我国武装力量的重要组成部分。武警理论研究、武警立法发展和武警执法实践都要求制定一部中国人民武装警察部队法。武警法是适用于武警部队的专门法,具有特殊性、专业性、独立性、分散性、交叉性的特点。武警法学具有自己独特的研究对象、研究方法、理论价值和科学体系,应该建构独立的武警法律学科,这是必然的发展趋势。     

一种结合弹道规律的模糊交互式多模型算法

针对交互式多模型算法中转移概率矩阵与实际运动不匹配而影响跟踪精度的问题,通过分析某型导弹的典型弹道,将弹道规律融合到模型概率转移矩阵中,然后将转移概率模糊化处理,提出了一种基于弹道规律的模糊交互式多模型算法,然后以导弹蛇形运动转至比例导引的机动过程为例进行了仿真验证,比较了典型交互式多模型算法和模糊交互式多模型算法的跟踪性能。仿真结果表明:该算法可显著提高导弹机动段的跟踪精度。     

基于BP和Hopfield神经网络的航空肼燃料保障安全评价

针对航空肼燃料保障安全评价的复杂性和非线性,提出并建立了基于BP和Hopfield神经网络的动态安全评价模型。在综合分析国内外肼燃料保障安全评价的基础上,针对航空肼燃料保障过程中出现的问题,构建并优化了指标体系,选取前馈神经网络中的BP网络和反馈神经网络中的Hopfield网络建立评价模型。在详细说明了BP和Hopfield神经网络的构建方法后,进行实例验证,并对预测效果进行了比较分析。仿真表明,两种模型都能正确评价安全保障状态。但在收敛速度、联想记忆功能方面Hopfield神经网络优于BP神经网络。将BP和Hopfield神经网络用于肼燃料保障安全评价过程中,具有适用性和可行性,对于航空肼燃料保障的安全建设与安全管理研究具有重要意义。     

Soldiers as victims: behind military barracks in the post-colonial African army

This paper examines the ways in which the military infringes on the social and political rights of soldiers who joined the Zimbabwe National Army in post-independence Zimbabwe. Contrary to the scholarly and policy debates that present Zimbabwean soldiers as the silent prop behind President Robert Mugabe and the perpetrators of political violence, this paper argues that these soldiers have also been victimised in army barracks. The victimhood of soldiers has been explicit in the ways in which they are forced to execute their duties beyond their professional expectations. In substantiating this argument, the paper explores the unethical military training and the ways in which soldiers are disciplined and punished through Chapter 11:02 of the draconian Defence Act. The paper’s contribution stems from a ‘rights’ perspective that emphasises the right to freedom, justice and protection, which is usually quite silent in the military. But the question is how can soldiers’ concerns be translated into new practices without compromising so-called ‘state security’?     

Scheduling combat logistics force replenishments at sea for the US Navy

The Replenishment at Sea Planner (RASP) is saving the U.S. Navy millions of dollars a year by reducing fuel consumption of its Combat Logistics Force (CLF). CLF shuttle supply ships deploy from ports to rendezvous with underway U.S. combatants and those of coalition partners. The overwhelming commodity transferred is fuel, ship‐to‐ship by hoses, while other important packaged goods and spare parts are high‐lined, or helicoptered between ships. The U.S. Navy is organized in large areas of responsibility called numbered fleets, and within each of these a scheduler must promulgate a daily forecast of CLF shuttle operations. The operational planning horizon extends out several weeks, or as far into the future as we can forecast demand. We solve RASP with integer linear optimization and a purpose‐built heuristic. RASP plans Replenishment‐at‐Sea (RAS) events with 4‐hour (Navy watch) time fidelity. For five years, RASP has served two purposes: (1) it helps schedulers generate a daily schedule and animates it using Google Earth, and (2) it automates reports command‐to‐ship messages that are essential to keep this complex logistics system operating.     

滑模控制的新型双幂次组合函数趋近律

提出一种基于双幂次组合函数趋近律的新型滑模控制方案。与现有的快速幂次或双幂次趋近律相比,具有更快的收敛速度,同时还保持了全局固定时间收敛特性,收敛时间上界与滑模初值无关。当系统存在有界扰动时,能够使滑模变量在有限时间内收敛到稳态误差界内,同时其稳态误差要小于现有方法的。仿真实验验证了该方法的有效性及理论分析的正确性。     

发动机冷却燃料超临界压力下做功潜力㶲分析

在高马赫数飞行下,超燃冲压发动机的燃料冷却量大于燃料燃烧量。为了降低燃料的冷却量以及实现燃料冷却量和燃烧量的匹配,采用分析法对超燃冲压发动机壁面燃料冷却工质在超临界压力下进行做功潜力分析。发动机壁面冷却燃料的特性决定其热量大小。根据发动机壁面温度分布、热流密度分布计算热量,建立稳定流动燃料工质的平衡方程。结果表明:在壁面最高温度为1200 K时,传入壁面的热量为562.4 k W,其中理论热量为541.3 k W;冷却燃料工质流量增加,最大输出功减小;燃料工质出口温度增加,输出功减小;燃料工质出口压力增加,输出功基本不变。