气动力/直接力复合导弹鲁棒控制器设计

提出了一种气动力/直接力复合控制导弹在舵机层面进行复合控制的鲁棒控制器设计方法,即空气舵与直接力喷流机构看作是复合舵系统模型.该方法在完成复合舵系统建模的基础上,利用参数空间方法对等效舵机系统进行设计,以确保在喷流因子变化时的鲁棒性.最后,通过仿真验证了该方法的可行性.     

先进的低特征信号推进剂研制

为了进一步提高导弹的突防能力和生存能力 ,扼要概括了国外战术导弹用低特征信号推进剂的现状 ;重点介绍了航天系统研制的几种不同能量梯次的低特征信号推进剂     

舰空导弹编队反导拦截决策模型

利用舰空导弹拦截反舰导弹的作战使用问题,是海军对空防御研究中的重要课题,而舰空导弹对反舰导弹的拦截决策又是此课题中的一个重要方面.立足于海军对空防御作战的实际需要,利用0-1整数规划的方法,研究编队在受到敌多发反舰导弹攻击情况下,舰空导弹对反舰导弹进行拦截的最佳拦截方案的统一优化决策模型.     

水面舰艇防御反舰导弹的技术途径

阐述了水面舰艇防御反舰导弹的各种技术途径.     

BALLISTIC TRAJECTORY

North Korea has been one of the world's most active suppliers of ballistic missile systems since the mid-1980s, but the nature of its missile export business has changed significantly during this period. Unclassified, publicly available data show that the great majority of known deliveries of complete missile systems from North Korea occurred before 1994. The subsequent fall-off took place a decade too early to be explained by the Proliferation Security Initiative of 2003. It can be explained by a combination of factors that have reduced demand. First, after selling production equipment for ballistic missiles to many states, especially in the Middle East, North Korea by the late 1990s had become primarily a supplier of missile parts and materials, not complete systems. Second, after Operation Desert Storm, some missile-buying states shifted their attention away from ballistic missiles in favor of manned aircraft, cruise missiles, and missile defense systems supplied by Western powers. Third, some states experienced pressure from the United States to curtail their dealings with North Korea. During the last decade, having shed most of its previous customer base, North Korea has entered a phase of collaborative missile development with a smaller number of state partners, particularly Iran and Syria. Its known sales of complete missile systems are relatively small and infrequent. North Korea's time as missile supplier to the Middle East at large has ended, but there is a risk that regional states will turn to North Korea as a supplier of nuclear technology in the future.     

弹道导弹关机点状态估计的指数加权递归最小二乘方法

在双星预警条件下,将指数加权递归最小二乘算法应用于目标关机点状态估计问题中。通过引入加权因子对目标助推段运动的局部拟线性特性进行描述,从而在一定程度上克服了一般的线性多项式模型难以准确刻画整个助推段运动的难题。通过对助推段目标动力学特性的分析,考察了目标在垂直射面方向上的运动特性。在此基础上,提出了一种更为准确的助推段运动模型。仿真算例表明,所提出的关机点状态估计方法相对于传统的方法具有一定的优越性。