浅议美军近距空中支援与空中遮断

美军近距空中支援与空中遮断在现代空战中发挥着十分重要的作用,已经成为了当前的热点研究方向。针对空中遮断理论研究相对较少的情况,以美军条令为参考,通过深入剖析二者的联系与区别,对比研究其组织体系与实施流程,有助于形成对空中遮断在作战理念、指挥控制、支援申请、作战运用等方面的系统认识,对丰富空中遮断理论和作战运用具有参考价值。     

美军反无人机技术装备发展解析

美军认为在可以预见的未来冲突及战争中,以无人机为典型代表的无人作战平台势将成为美军必须应对的主要挑战.在此背景下,美军以其作战使命的未来调整为核心着眼点,有效依托美国防工业界的技术研发力量,加快推动反无人机武器系统的研制、测试与升级,逐渐探索出了一条独具特色的反无人机技术装备发展之路.首先阐释了美军对无人机威胁的基本认识,其后对美军反无人机技术装备发展现状加以归纳梳理,最后分析总结了美军反无人机技术装备发展的主要特点.     

美军电磁频谱领域的发展

为谋求联合作战介入背景下的电磁频谱优势,抵消对手日益增强的“反介入/区域拒止”能力,美军不断推出并持续完善相关电磁频谱概念,利用电磁频谱开展态势感知、信息共享、作战协同、压制对抗等行动。通过梳理美军电磁频谱领域的发展脉络,分析美军在电磁频谱领域的发展特点和先进举措。     

伴飞诱饵支援条件下无人飞行器协同作战效能研究

针对复杂的威胁环境，介绍了伴飞诱饵在体系作战条件下的应用情况；基于排队论的突防概率模型，研究了伴飞诱饵支援条件下，无人飞行器的协同突防概率和效费比：提出了作战体系作战时效性的概念；建立了火力对抗条件下无人飞行器打击防空导弹防御体系的Lanchester方程，利用所建模型分析了伴飞诱饵对作战时效性的贡献。研究表明，排队论和Lanchester方程用于伴飞诱饵条件下的无人飞行器协同作战效能研究是有效的。     

美军作战仿真系统综述

电子信息装备是武器装备体系的中枢,作战仿真技术是评估装备作战效能、提升部队作战训练效果的重要手段。以处于世界领先地位的美军作战仿真系统为研究对象,从介绍美军仿真的分类图谱、分析其技术体系发展过程入手,重点阐述了美军典型联合作战仿真系统的功能定位、组成及应用情况,介绍了美军作战仿真系统的成功经验及其技术局限性。     

海上编队区域防御面临的新威胁和对策(下)

正3.美国海空军的威胁分析美国海空军是世界上最强大的军事力量,为了保持其军事优势,正在加速进行新军事变革。随着美国海空军新型装备的研制,美国海空军反舰作战的指导思想和作战手段将发生重大变化。一是实施联合作战。"联合能力"是美军未来建设的重点,最终要实现部队的"无缝联合",进行一体化作战。二是实施远程打击。未来,美军空中力量要能在全天候条件下摧毁移动目标,并     

美军电磁频谱作战装备及其作战应用分析

近年来,美军不断推进传统电子战向电磁战进而向电磁频谱作战转型,通过发布新战略新条令、重构组织机构、研发新技术和部署新装备等手段,构建更强大的电磁频谱作战能力。从美军电磁频谱作战概念发展入手,梳理美军正在大力发展的典型电磁频谱作战装备,总结其发展趋势,分析其作战应用模式。     

敏捷作战思想下导弹创新发展途径系统研究

敏捷作战(Operational Agility)亦称作战敏捷性,由美国空军在2015年9月发布的《2035年美国空军未来作战概念》中提出,是美军在原有作战概念基础上的融合创新,将对导弹武器的发展和美军新型作战能力的生成产生重要影响。本文基于敏捷作战思想,剖析其提出的背景与内涵,研究其对导弹作战运用的需求,并系统分析敏捷作战思想下导弹创新发展的途径和重要问题。     

美军一体化联合作战体系构建方法简析

正一、美军一体化联合作战的概念形成美军联合作战概念的正式提出至今已经25年,最初是军兵种自下而上的联合作战,2003年提出了联合一体化的概念,将联合作战概念内涵推演至跨军种白上而下一体化联合作战样式,2012年以后发布的联合作战文件,又将一体化概念提升到跨域协同作战样式。1.联合作战概念的初级阶段美军联合作战思想最早在20世纪70年代末、80年代初伴随着陆军提出"空地一体战"作战理论而     

国外导弹防御体系的现状与发展趋势

随着高技术特别是信息技术在军事领域的广泛应用,空中力量获得了飞速发展。空中力量的进攻作战能力大大提高,空战战法更为灵活多变,使高技术条件下的防空作战面临着越来越严峻的挑战。分析了信息化作战条件下现代防空体系面临的威胁,对美国、俄罗斯导弹防御体系的发展现状及发展趋势进行了分析和研究。     

On the stability of the track of the space elevator

A string moving with geostationary angular velocity in its radial relative equilibrium configuration around the Earth, reaching from the surface of the Earth far beyond the geostationary height, could be used as track for an Earth to space elevator. This is an old dream of mankind, originating about 100 years ago in Russia. Besides the question of feasibility from a technological point of view also the question concerning the stability of such a configuration has not yet been completely solved. Under the assumption that a proper material (carbon nanotubes) is available, making the connection possible technologically, we address the question of existence and stability of the radial relative equilibrium of a tapered string on a circular geosynchronous trajectory around the Earth, reaching from the surface of the Earth far beyond the geostationary height.     

On the Possibility of the Existence of Volatile Compounds in the Region of the Scott Crater on the Moon

In this paper, we analyze the illumination conditions, the thermal regime, and the possibility of deposits of volatile compounds existing in the vicinity region (NSR S5 region) near the southern pole of the Moon. It has been found that there are no permanently shadowed zones near the Scott crater and the NSR S5 region, though the temperature conditions allow the of compounds such as CH₃OH, SO₂, NH₃, CO₂, H₂S, C₂H₄, and water to remain stable relative to evaporation for a long time (≥1 Gyr). It has been also shown that compounds like CO and CH₄ cannot stably exist in these regions.     

Estimation of the current density and analysis of the geometry of the current system surrounding the Earth

The results of an investigation of the distribution of plasma pressure, pressure gradients, and magnetic field near the equatorial plane in the plasma ring surrounding the Earth under magneto-quiet conditions are presented. Observational data obtained during the international THEMIS mission are used. The picture of the distribution of transverse-current density near the equatorial plane was obtained under assumption of observing the magnetostatic balance condition at geocentric distances from 6 to 12R _E. In estimating the integral transverse current it was accepted that in daytime sector the magnetic-field minima on magnetic field lines are not localized in the equatorial plane. Estimates of the integral transverse current were obtained, which demonstrate the possibility of closing nighttime transverse currents at geocentric distances of up to ～12R _E inside the magnetosphere, which form a high-latitudinal continuation of the ring current.     

对老年人体育锻炼负荷量监控方法的探讨

通过对老年人体育锻炼活动的情况进行相关调查，发现目前老年人体育锻炼中存在一些误区。因此本文针对这些现实情况提出，应根据实际情况运用一些简单易行的方法来对老年人体育锻炼实施医务监督，达到提高老年人体育锻炼的科学性。     

Estimating the accuracy of the technique of reconstructing the rotational motion of a satellite based on the measurements of its angular velocity and the magnetic field of the Earth

The paper has studied the accuracy of the technique that allows the rotational motion of the Earth artificial satellites (AES) to be reconstructed based on the data of onboard measurements of angular velocity vectors and the strength of the Earth magnetic field (EMF). The technique is based on kinematic equations of the rotational motion of a rigid body. Both types of measurement data collected over some time interval have been processed jointly. The angular velocity measurements have been approximated using convenient formulas, which are substituted into the kinematic differential equations for the quaternion that specifies the transition from the body-fixed coordinate system of a satellite to the inertial coordinate system. Thus obtained equations represent a kinematic model of the rotational motion of a satellite. The solution of these equations, which approximate real motion, has been found by the least-square method from the condition of best fitting between the data of measurements of the EMF strength vector and its calculated values. The accuracy of the technique has been estimated by processing the data obtained from the board of the service module of the International Space Station (ISS). The reconstruction of station motion using the aforementioned technique has been compared with the telemetry data on the actual motion of the station. The technique has allowed us to reconstruct the station motion in the orbital orientation mode with a maximum error less than 0.6° and the turns with a maximal error of less than 1.2°.     

实施“三位一体”教育模式 提高学生的综合素质

本文介绍了“三位一体”教育模式的内容,描述亍我们实施该模式所采取的措施及取得的成效。实践表明,“三位一体”教育模式能够提高学生的综合素质,为学生毕业后的发展打下坚实基础,对教育模式的改革具有一定的指导意义。     

从应变计现状看电阻式传感器的前景

电阻式传感器的核心部件——电阻应变计是目前最常用的应力分析的敏感元件。也常用于测量力、压力、扭矩和加速度等物理量。作者简要回顾了电阻应变计的发展历史，介绍了电阻应变计的结构、分类及现状，展望了电阻式传感器的前景。     

System of works on numerical modeling of the dynamics of the structure of the Space Radiotelescope in the RadioAstron project

The results of modeling the dynamics of the Space Radiotelescope are presented. The results of ground-based vibration-dynamic tests are used to validate the calculation models and estimate the damping levels. The dynamic distortions of the reflecting surface caused by the operation of the pointing mechanism of the high-gain antenna are estimated.     

Optimization of the trajectory of the spacecraft insertion into the system of heliocentric orbits

The possibility of the spacecraft insertion into the system of operational heliocentric orbits has been analyzed. It has been proposed to use a system of several operational heliocentric orbits. On each orbit, the spacecraft makes one or more revolutions around the Sun. These orbits are characterized by a relatively small perihelion radius and relatively high inclination, which allows one to investigate the polar regions of the Sun. The transition of the spacecraft from one orbit to another has been performed using an unpowered gravity assist maneuver near Venus and does not require the cruise propulsion operation. Each maneuver transfers the spacecraft into the sequence of operational heliocentric orbits. We have analyzed several systems of operational heliocentric orbits into which the spacecraft can be inserted by means of the considered transportation system with electric propulsion (EP). The mass of the spacecraft delivered to these systems of operational orbits has been estimated.     

火箭推进剂液体晃动关机响应的数值仿真

本文采用VOF方法对火箭发动机关机阶段所引起的液体晃动进行了数值仿真，以氧化剂贮箱为例，得到了贮箱无阻尼环和带阻尼环时的晃动仿真图和液体质心变化曲线，检验了VOF方法处理碎波的能力。