地球扰动引力对弹道导弹命中精度影响的等效补偿理论

为消除地球扰动引力的影响、提高弹道导弹的命中精度,根据地球扰动引力对弹道导弹运动影响的特性与控制系统理论,建立不直接补偿地球扰动引力对导弹运动参数的影响却能满足命中精度要求的等效补偿理论。根据不同补偿方式与补偿量的特点,提出嵌入式、分步式、分段式等补偿模式,为补偿地球扰动引力对导弹运动的影响提供了一个通用框架和理论基础。     

Military expenditure and economic development in China: an empirical inquiry

Increases in military spending have a big impact on the socioeconomic conditions in any country. However, there is no consensus as to whether the rising military expenditure is beneficial or detrimental to economic growth. The present study chose China as a case study to empirically examine a complex relationship between military expenditure and economic development. The findings from the Johansen cointegration test indicated that there existed a long-run relationship between China’s military spending and economic growth. Furthermore, the Granger causality test detected a unidirectional causality from economic development to military expenditure. These results were further confirmed by the findings from the impulse response function. This means that China represents an example of a developing economy where the size of military expenditure expands in the process of economic transformation.     

反潜无人艇军事需求与作战模式

本文分析了反潜无人艇在打造新型水下作战体系、夺取水下空间控制权中的现实军事需求,对反潜无人艇担负的作战任务及典型作战模式进行研究,并针对任务实际提出了反潜无人艇的能力需要。     

论当今国际维和行动发展和趋势

本文从当今国际维和行动现状出发,分析了国际维和行动的特点,剖析了国际维和行动面临的挑战问题,最后对国际维和行动的发展提出几点思考,并系统阐述了维和行动的相关问题。     

复合型科学家：颠覆性创新产品研发的灵魂

科学探索是颠覆性技术创新产品的源泉,复合型科学家为颠覆性创新产品开辟方向、提供战略咨询、构建技术原理或设计方案、直接研制创新产品。本文提出,要高度重视复合型科学家的主导地位,加大育才引才留才力度,营造发挥才华的包容性科学文化环境。     

Integrated guidance and control of guided projectile with multiple constraints based on fuzzy adaptive and dynamic surface

Based on fuzzy adaptive and dynamic surface (FADS), an integrated guidance and control (IGC) approach was proposed for large caliber naval gun guided projectile, which was robust to target maneuver, canard dynamic characteristics, and multiple constraints, such as impact angle, limited measurement of line of sight (LOS) angle rate and nonlinear saturation of canard deflection. Initially, a strict feedback cascade model of IGC in longitudinal plane was established, and extended state observer (ESO) was designed to estimate LOS angle rate and uncertain disturbances with unknown boundary inside and outside of system, including aerodynamic parameters perturbation, target maneuver and model errors. Secondly, aiming at zeroing LOS angle tracking error and LOS angle rate in finite time, a nonsingular terminal sliding mode (NTSM) was designed with adaptive exponential reaching law. Furthermore, combining with dynamic surface, which prevented the complex differential of virtual control laws, the fuzzy adaptive systems were designed to approximate observation errors of uncertain disturbances and to reduce chatter of control law. Finally, the adaptive Nussbaum gain function was introduced to compensate nonlinear saturation of canard deflection. The LOS angle tracking error and LOS angle rate were convergent in finite time and whole system states were uniform ultimately bounded, rigorously proven by Lyapunov stability theory. Hardware-in-the-loop simulation (HILS) and digital simulation experiments both showed FADS provided guided projectile with good guidance performance while striking targets with different maneuvering forms.     

当代俄罗斯电子战产品主要研制单位及装备发展综述

作为现代战场的核心内容之一,无线电电子战产品已成为近几十年来发展异常迅速的一类军事装备。俄罗斯的军事装备历经车臣战争、俄格冲突、叙利亚战争和俄乌冲突等众多实战检验并不断得到完善,正逐渐展现出强大的军事威慑力,而电子战设备就是俄罗斯重点发展且成效显著的“不对称”战力方向之一。西方专家普遍认为电子战系统是俄军最危险的武器装备之一,可见其水平已属国际领先水平。本文介绍了当代俄罗斯对无线电电子战内容的理解、俄罗斯电子战产品的主要研制单位和发展现状,重点分析了俄罗斯近30年来最知名的陆、海、空电子战装备的分类、组成、指标和功能等,对俄罗斯电子战未来的技术发展趋势进行了预测,以期为国内电子战装备和技术发展提供借鉴。     

美军作战概念开发特点及启示

创新军事思想、开发作战概念是推进军事转型和部队建设的关键抓手。美军秉承“创新提炼—集智研讨—实验验证”的作战概念开发机制,采取聚焦联合作战概念开发,以作战能力需求为牵引,通过突破前沿技术和研发关键装备,以法规制度和标准规范为强制约束的做法对于军队转型建设具有重要启示。本文提出,应着眼于军队的使命任务,强化军队作战概念设计,创新作战概念研究方式,形成“聚焦使命任务—研讨演示概念—体系设计概念—检验优化概念—形成概念产品—指导建设实践”的作战概念开发途径,支撑作战概念创新和前瞻性探索研究,并加强体制机制和标准规范建设,通过对作战概念开发的整体设计和约束规范,提升前瞻作战概念对作战实践的创新引领作用,加速推进军队转型建设。     

轴向输出TE10模式的紧凑型相对论磁控管的粒子模拟

研究了一种轴向输出TE10模式的紧凑型相对论磁控管,该器件采用6谐振腔结构并工作在π模式上,通过4腔轴向输出的结构设计使得谐振腔结构与矩形输出波导之间形成了较好的过渡,实现了矩形TE10模式的微波输出。与衍射输出相对论磁控管相比,这种结构设计不仅能减小磁控管的轴向和径向的尺寸,使得系统更加紧凑化,而且能在输出波导中获得更加纯净的低阶微波模式。利用粒子模拟软件,初步分析和优化了器件的工作性能。模拟结果表明:当电压为500k V,磁场为0.5T时,该器件的工作频率为2.58GHz,输出功率为1.0GW,功率转换效率达到25.0%。     

近距格斗规避方式研究

空中格斗过程中,当歼击机处于有利位置时,飞行员应操纵歼击机进行机动飞行以便能采用一定的攻击方式攻击目标飞机,当飞行员判断出空战态势对其不利时,往往采用一定的规避机动方法躲避敌机的跟踪和攻击。文中重点阐述了歼击机在空对空格斗状态下常用的几种规避机动方式:逃逸法、保持航向正切法和终端消极偏差法,给出了其定义,分析了其主要的运动特征,并对规避路线运动学方程及边界等运动特性进行了一定的研究。