基于双滑模变结构的旋转靶弹双通道控制

针对旋转靶弹低空飞行姿态难以快速调整以及参数摄动的问题,基于内外环的双滑模变结构方法,设计了旋转靶弹的双通道控制器。基于非线性模型,对靶弹快速变化的攻角和侧滑角以及慢速变化的高度和偏航距离分别设计了一种积分型滑模面,并采用指数趋近律减轻系统的抖振,利用Lyapunov稳定理论证明其稳定性。非线性仿真结果表明,该设计控制方法能快速准确响应控制指令,且在参数摄动时表现出较强的鲁棒性。     

可变搜索区末制导雷达捕捉模型

反舰导弹远程化是一种发展趋势。但是随着射程的增加,反舰导弹自控终点的误差散布也增加,同时降低了目标捕捉概率,扩大末制导雷达搜索区域是解决该问题的一个途径,但这将降低末制导雷达的目标选择能力。选用可变搜索区末制导雷达是解决该矛盾的一种方法。在分析该模式末制导雷达搜索规律的基础上,建立了可变搜索区末制导雷达目标捕捉模型,为该模式末制导雷达目标捕捉概率的计算提供了一种较准确的方法。仿真结果显示该模型基本可信。     

导弹气动参数变化时PID与模糊控制的仿真

以参数大范围变化的导弹为研究对象,分别设计PID控制器和模糊控制器,并对PID控制器和模糊控制器组成的稳定回路进行仿真,仿真结果表明,PID控制器不能适应参数大范围的变化,表现为容易产生超调。简单模糊控制器对外界参数具有较好的适应性和鲁棒性,但存在稳态误差,通过采取模糊——积分并联混合,改善了模糊控制的稳态性能,提高了模糊控制的稳态精度。     

基于飞行时间的弹道导弹火力控制

为了达到最佳射击效果,弹道导弹突击目标时经常需要多枚导弹同时击中目标,因此根据飞行时间确定发射时间则成为弹道导弹火力控制问题的重要内容。以具体导弹为例,采用仿真的方法分析了影响飞行时间的内在原因,得出了明确的结论,使导弹部队能够根据飞行时间确定发射时间,从而合理地进行火力控制,提高毁伤效果和震慑力。     

多机空战系统的歼击机建模技术

分析了多机空战系统的顶层模型结构,给出了机载雷达、武器控制和导弹等三个主要部件的模型,可以将其应用于多机空战仿真系统的数学建模和软件设计中.     

导弹子母弹战斗部对复杂目标毁伤的计算机仿真

介绍了蒙特卡洛方法(Monte-Carlo)仿真的基本原理,并运用该方法对导弹子母弹战斗部对复杂目标毁伤进行研究,利用Matlab语言编制仿真程序实现了计算机仿真.有效地解决了其他方法计算繁琐的弊端,大大提高了毁伤仿真的计算效率.仿真结果表明应用该方法建模技术简洁,模型的通用性好,并能够随时根据需求进行功能扩展.     

A split target detection and tracking algorithm for ballistic missile tracking during the re-entry phase

In the re-entry phase of a ballistic missile, decoys can be deployed as a mean to overburden enemy defenses. This results in a single track being split into multiple track-lets. Tracking of these track-lets is a critical task as any miss in the tracking procedure can become a cause of a major threat. The tracking process becomes more complicated in the presence of clutter. The low detection rate is one of the factors that may contribute to increasing the difficulty level in terms of tracking in the cluttered environment. This work introduces a new algorithm for the split event detection and target tracking under the framework of the joint integrated probabilistic data association (JIPDA) algorithm. The proposed algorithm is termed as split event-JIPDA (SE-JIPDA). This work establishes the mathematical foundation for the split target detection and tracking mechanism. The performance analysis is made under different simulation conditions to provide a clear insight into the merits of the proposed algorithm. The performance parameters in these simulations are the root mean square error (RMSE), confirmed true track rate (CTTR) and confirmed split true track rate (CSTTR).     

导弹结构热防护一体化设计与优化

针对导弹面临的严酷气动热力环境,基于传统波纹夹芯结构,为导弹设计了一种兼具承载和热防护功能的一体化结构。建立热-结构耦合计算模型,对一体化结构进行结构承载与热防护性能分析,结果表明:一体化结构在高温下具有较好的承载能力;增加一体化结构隔热层与内壁厚度有助于提高导弹的热防护效率。以一体化结构热防护效率最高和质量最小为目标,采用第二代非支配排序遗传算法实现了多目标优化,并认识到:一体化结构热防护效率与质量相互影响,设计时需要需综合考虑。     

舰载充气式角反射体反导装备发展及运用

为提高我国电子战反导水平和导弹突防能力,根据电子战反导装备发展趋势,分析舰载充气式角反射体的反导原理,介绍舰载充气式角反射体反导装备的发展情况,论证了充气式角反射体迷惑、冲淡、转移和质心式干扰的运用。对电子战反导装备的发展以及部队战法研究具有一定理论意义和参考价值。     

Multilateral defense cooperation in the Indo-Asia-Pacific region: Tentative steps toward a regional NATO?

Some U.S. military leaders have asserted that the United States, Japan, Australia, and India and the Republic of Korea are developing multilateral defense cooperation to deter aggression and uphold norms much like North Atlantic Treaty Organization (NATO) has in Europe. Frequent military exercises and China’s threats to freedom of navigation (FoN) and North Korea’s nuclear missiles comprise the motive force for such cooperation. However, cooperation thus far has been trilateral and minimal, given divergent national interests and dispersed geopolitical locations. Cooperation among Japan, Republic of Korea (ROK), and the United States is increasing given the threat, but ROK’s public opinion is divided about Japan. Australia, Japan, and India have increased cooperation with the United States but are reluctant to conduct FoN operations with the United States to challenge China’s expansionism in the South China Sea. If China becomes more aggressive and blocks FoN or seizes territory, development toward an Asian NATO is possible.