能量均衡的围捕任务分配方法

随着水下机器人反围捕策略研究的不断深入,水下机器人围捕变得越来越困难。为此构建一种多层环状伏击围捕模型并设计了基于围捕任务的任务分配方法,使得水下机器人能够充分利用自身的特点更好地完成任务。同时,考虑在围捕过程中随时间推移,系统内能量会出现消耗不均的现象,据此提出一种能量均衡方法平衡系统能量的消耗。实验证明所提出的基于多层环状围捕模型的能量均衡策略任务分配方法能有效提高围捕成功率,延长系统寿命。     

Revisiting the justification for an all-volunteer force

In 1968, President Nixon established the Commission on an All-Volunteer Armed Force, or the Gates Commission, which served as the impetus and justification for an All-Volunteer Force (AVF). At the end of its deliberations, the commission recommended abolishing the draft and transforming the U.S. military into a force of volunteers beginning in 1973. Interestingly, the debate regarding the merits of both systems appeared to be largely economic – with cost–benefit analysis playing the primary role. Lately, we are beginning to see a new, politically-motivated impetus for returning to a “system of national service.” The ideas spurring this debate are many: the need to reaffirm the nation state, the commitment of citizens to the state, political ownership and oversight of the forces, the need for social equity in serving the nation, limiting the support for armed conflict by burden-sharing among citizens, and equitably spreading the personal cost of war.     

Northern Ireland and minimum force: the refutation of a concept?

The debate over whether there exists a British counter-insurgency tradition of minimum force is one that has been thoroughly discussed. Is there anything left to say? This study suggests there is further insight to be attained if one explicitly evaluates the concept of minimum force in relation to the conduct of the security forces in the years of the Northern Ireland conflict. Through an examination of three key periods in the conflict, it will be shown that while there was invariably an awareness of the need to act with restraint among senior officers at the strategic level, this was often difficult to apply at the tactical level in the heat of confrontation. The argument demonstrates that the British Army, and other instruments of the state, rarely acted in a manner that could be described as ‘minimal’. Instead, it was the broader liberal values of the British state that explains largely the degrees of restraint exhibited by the government and security forces.     

The ‘first’ surge: the repulse of the Easter Invasion in South Vietnam, 1972 – implications for Iraq and Afghanistan

In a military intervention, do surges work? I compare the failed ‘surge’ in Vietnam, the repulse of the Easter Invasion in 1972, as a means of assessing the more ambiguous surges in Iraq and Afghanistan. I identify four features of a surge for this analysis: the military dimensions and strategy of the surging forces, the military capabilities of the host forces, the political vitality and will of the host country, and the political commitment in the domestic politics of the intervener. I find that the last feature is the most critical; and, in all three surges, the American political commitment was lacking.     

尾空泡对水下航行体流体阻尼力影响数值研究

针对航行体尾空泡对流体阻尼力影响问题,结合动坐标系技术和空泡多相流数值模拟方法,通过求解雷诺平均的NS方程组,进行了阻尼力计算研究。通过与试验数据对比,表明该方法具有较好的精度。数值计算研究表明,尾空泡会削弱航行体尾部压力的不对称性,使航行体尾部流体阻尼力减小。当尾空泡增加到一定尺寸时,流体阻尼力减小幅度逐渐趋缓,同时尾空泡也改变了流体阻尼力随攻角的变化趋势。研究充分表明了航行体流体力设计中考虑尾空泡影响的必要性。     

有限质量降落伞充气动力学数值模拟

为研究空投任务中降落伞有限质量充气过程的动力学行为,基于罚函数耦合方法和网格自适应技术分析了降落伞柔性结构与周围不可压缩流场的流固耦合特性。数值模拟开伞过程伞衣三维外形变化,获得降落伞系统下落速度、阻力面积等参数;对比分析初始投放速度对降落伞开伞时间、伞衣阻力面积的影响;通过试验数据对比分析开伞力变化。计算结果表明,该方法可以有效模拟降落伞系统有限质量充气过程的动力学特性,仿真结果与试验结果相符。     

尾空泡对水下航行体流体阻尼力影响数值计算分析

针对航行体尾空泡对流体阻尼力影响的问题,结合动坐标系技术和空泡多相流数值模拟方法,通过求解雷诺平均的纳维-斯托克斯方程组,进行阻尼力计算研究。试验数据对比结果表明,该方法具有较好的精度。数值计算研究表明,尾空泡会削弱航行体尾部压力的不对称性,使航行体尾部流体阻尼力减小。当尾空泡增加到一定尺寸时,流体阻尼力减小的幅度逐渐趋缓,同时尾空泡也改变了流体阻尼力随攻角的变化趋势。研究充分表明了航行体流体力设计中考虑尾空泡影响的必要性。     

基于UML的美军动能反卫作战系统概念建模

针对美军动能反卫作战系统,利用UML方法,对其作战仿真概念建模进行了初步的探讨。针对作战系统的反卫作战任务,首先识别系统的主要行为,利用用例图定义系统的功能需求;其次利用类图标识系统用例模型中的所有实体,并分析这些实体的关联关系;最后,采用顺序图展示对象在系统执行过程中不同阶段的动态交互。这样建立的概念模型描述规范,为下一步仿真系统的开发奠定了良好知识表示基础。     

转管炮降低机心组导轨摩擦力研究

为了使转管炮机心组消耗的驱动功率最小,对机心组速度、主滚轮相对机体位置、机心体左右导轨及倾角关系等对驱动功率的影响进行研究。表明最好选用机心组凸轮加速度最小,主滚轮相对机体质心位置等于零,最好用无横向位移以及有夹角的关系最好。优化结果表明:9 000 rpm的射速,驱动功率由机心组加速度变化引起140kw下降到31 kw,降到不足于原设计曲线的22%;射速为3 300 rpm的主滚轮压力峰值参数化峰值1 086.5 N,升高到10 000 rpm的峰值9 779.3 N。无横向以及有夹角降低压力有横向以及无夹角90.9%。     

美国电磁轨道发射技术现状及特点分析

以电磁轨道炮为主,介绍美国陆、海军电磁轨道发射技术的发展历程及阶段性研究成果、发展目标与未来规划、研究机构及相关研究方向、潜在应用领域以及近期电磁轨道炮的主要战术技术指标,并对其关键技术特点进行了分析。