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21.
组播技术的应用可以有效提高RTI的实现性能。介绍了组播分配的一般理论和实现方案,详细展示了KD RTI中的组播分配策略,讨论了组播应用过程中出现的问题,同时给出了解决方法。  相似文献   
22.
在满足对目标卫星在指定时间进行拦截的要求下,考虑拦截器变轨能量消耗最省,提出了基于定时拦截的在轨机动拦截轨道选择与优化方法。该方法能够迅速设计和优化出最优在轨机动拦截轨道、变轨点位置和变轨所需的能量。仿真结果表明,模型准确、有效,能够满足作战要求。  相似文献   
23.
This paper contributes to the growing literature on the milex-growth nexus, by providing a case study of South Africa and considering the possibility of structural breaks by applying newly developed econometric methods. Using full sample bootstrap Granger non-causality tests, no Granger causal link is found between military expenditure and GDP for 1951–2010, but parameter instability tests show the estimated VARs to be unstable. Using a bootstrap rolling window estimation procedure, however, finds evidence of bidirectional Granger causality in various subsamples. This implies standard Granger non-causality tests, which neither account for structural breaks nor time variation may be invalid.  相似文献   
24.
We investigate whether differences in terrorism risk are mirrored on terrorism risk perception across European countries for the period 2003–2007. We find that the average propensity for terrorism risk concern is affected by actual risk levels. Country and individual heterogeneity contribute substantially to the variation of observed risk perception. Singles and individuals with white collar jobs are less likely to mention terrorism as one of the most pressing issues their country faces, while political positioning towards the right makes it more likely to be concerned about terrorism. As far as competing risks are concerned, we find that the likelihood terrorism is mentioned, decreases with spending on pensions as a percentage of GDP being higher. Finally, based on the Bayesian framework, we also examined the formation of terrorism risk perceptions, and decompose the observed country-level time series of terrorism activity into a long- and a short-run component. We concluded that the observed risk perception variation is only explained by the long-term trend of terrorism activity countries face.  相似文献   
25.
机载有源雷达干扰系统是现代飞机一种辅助电子对抗系统,根据其功能可分为支援干扰系统和自卫干扰系统,其中支援干扰系统装在专用电子战飞机上,自卫干扰系统装在作战飞机吊舱上.主要论述国外机载电子干扰吊舱的构成、装载平台、技术现状及发展.  相似文献   
26.
基于排队论的防空导弹群作战效能研究   总被引:1,自引:0,他引:1  
结合防空导弹群防空战斗的特点,利用可列状态生灭过程的排队论方法,研究了防空导弹群作战效能,建立了数学模型,分析了导弹群防空武器系统对目标平均击毁概率的计算方法,并通过引入拦截适宜性因子对理想条件下的排队模型进行了修正,为类似问题的研究提供了一种参考。  相似文献   
27.
网络化无人水下航行器CAN总线调度方法   总被引:3,自引:0,他引:3  
传感器时间驱动,控制器和执行器均为事件驱动的网络控制系统节点驱动方式,已在众多的网络控制系统研究中被采用。在此种节点驱动方式下,依据各控制回路传感信息的不同时间性质将网络化无人水下航行器各控制回路划分为周期性控制回路和随机性控制回路来进行处理。采用时分复用原理对系统总线传输时间进行划分,通过递归遍历寻优方法对系统周期性控制回路信息传输需求进行优化调度;基本周期最小时间余量最大的寻优指标确保了总线负载均衡和随机性控制回路信息传输需求得到及时满足,这样有效地减少了低优先级控制回路(节点)信息传输的延迟等待时间。利用M ATLAB/T uretim e工具进行仿真试验,仿真结果说明了调度方法的有效性。  相似文献   
28.
This paper offers the personal view of a senior executive in the Defence Procurement Agency about the future requirements of the defence industry’s principal UK customer. The focus here is on trying to identify the type of corporate behaviour and range of skill sets that the UK Government will need from defence suppliers, both primes and supply chain companies in the future. The concluding message from this ‘Customer View’ is that there is likely to be a continuing market for the company that specializes in delivering defence capability. It will be a company that will be looking for a long‐term relationship, with a specialist knowledge of its various national customers and a willingness to work openly and closely with them. It will be agile in its ability to bring together diverse technologies, to package them as a system and to deliver them either as hardware or as a service. Such suppliers will also need to innovate and to adapt at least as rapidly as the threats that they seek to counter.  相似文献   
29.
根据时域有限差分法(Finite Difference Time Domain, FDTD)的基本原理,本文首先分析了等离子体的物理场特性及数值计算,然后介绍了飞行器再入时等离子鞘的形成以及等离子体相对介电常数对波的衰减,最后通过三维FDTD和二维FDTD模拟了电磁波在等离子体中的传播情况,证明了FDTD方法是解决电磁波在复杂媒质中传播的一种有效方法,并探究了飞行器再入段黑障区通信的理论和方法。  相似文献   
30.
《防务技术》2022,18(12):2170-2180
The reconstruction control of modular self-reconfigurable spacecraft (MSRS) is addressed using an adaptive sliding mode control (ASMC) scheme based on time-delay estimation (TDE) technology. In contrast to the ground, the base of the MSRS is floating when assembled in orbit, resulting in a strong dynamic coupling effect. A TED-based ASMC technique with exponential reaching law is designed to achieve high-precision coordinated control between the spacecraft base and the robotic arm. TDE technology is used by the controller to compensate for coupling terms and uncertainties, while ASMC can augment and improve TDE’s robustness. To suppress TDE errors and eliminate chattering, a new adaptive law is created to modify gain parameters online, ensuring quick dynamic response and high tracking accuracy. The Lyapunov approach shows that the tracking errors are uniformly ultimately bounded (UUB). Finally, the on-orbit assembly process of MSRS is simulated to validate the efficacy of the proposed control scheme. The simulation results show that the proposed control method can accurately complete the target module’s on-orbit assembly, with minimal perturbations to the spacecraft’s attitude. Meanwhile, it has a high level of robustness and can effectively eliminate chattering.  相似文献   
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