对三个宇宙速度的另一种推导

高中新编物理教材(试验修订本·必修)在"人造卫星宇宙速度"一节中,只对第一宇宙速度进行了推导,而在课文中介绍了第二宇宙速度和第三宇宙速度.有的学生问老师:"第二、第三宇宙速度是如何推导出来的,请老师告诉我们的推导方法."如果一句话回答说:"你们的数学知识还不够,现在还不能推导."那么学生不仅是很扫兴,而且会失去对老师的信任.笔者在教学过程中,与学生共同探讨了另一种推导三个宇宙速度的方法,现介绍如下,供参考.     

挠性联结双体卫星的混沌运动

本文讨论一挠性联结双刚体航天器模型，通过计算其动力学方程异宿轨道稳定流形与不稳定流形的相交角方法，给出其稳定流形与不稳定流形横截相交的判据，并通过Ｐｏｉｎｃａｒｅ截面的计算，证明其产生混沌运动的可能性。     

声悬浮技术的发展及应用

<正>一、引言在过去半个世纪中,空间技术的发展日新月异。人们先后实现了人造卫星的发射,太空漫步和空间站的建立。空间环境与地面条件有着显著的不同,其主要特征有微重力、无容器、超高真空和宇宙射线等。如何利用空间环境进行科学研究和材料制备成为国际热点课题。美国、俄罗斯、欧盟、中国和     

Solution set on the natural satellite formation orbits under first-order earth＇s non-spherical perturbation

Using the reference orbital element approach, the precise governing equations for the relative motion of formation flight are formulated. A number of ideal formations with respect to an elliptic orbit can be designed based on the relative motion analysis from the equations. The features of the oscillating reference orbital elements are studied by using the perturbation theory. The changes in the relative orbit under perturbation are divided into three categories, termed scale enlargement, drift and distortion respectively. By properly choosing the initial mean orbital elements for the leader and follower satellites, the deviations from originally regular formation orbit caused by the perturbation can be suppressed. Thereby the natural formation is set up. It behaves either like non-disturbed or need little control to maintain. The presented reference orbital element approach highlights the kinematics properties of the relative motion and is convenient to incorporate the results of perturbation analysis on orbital elements. This method of formation design has advantages over other methods in seeking natural formation and in initializing formation.     

USEFUL RELATIVE MOTION DESCRIPTION METHOD FOR PERTURBATIONS ANALYSIS IN SATELLITE FORMATION FLYING

Nomenclature OXYZEarth’sequatorialinertialreferenceframeωArgumentofperigee SlxyzLeadingsatelliteorbitframeMMeananomaly SfxyzFollowingsatelliteorbitframefTrueanomalyaSemi majoraxisθ=ω fArgumentoflatitude eEccentricitynMeanmotion iOrbitinclinationrSatel…     

卫星热设计参数的灵敏度分析

卫星热设计参数的灵敏度分析为卫星热设计的可靠性验证以及卫星运行可靠性提供了分析方法．利用系统灵敏度理论，对卫星热设计问题进行了分析，导出了卫星热设计系统的灵敏度方程．并以太阳能电池板的热设计为例，对系统的灵敏度方程进行了求解，分析了各参数的灵敏度，为卫星热设计中结构及物性参数的确定提供了依据。     

运载火箭和航天飞机

人造卫星要有运载工具把它送入空间预定轨道．目前使用的运载工具主要有运载火箭和航天飞机．运载火箭是一次性使用，无人驾驶；航天飞机可多次使用，一般有人驾驶．下面对它们的原理、构造、发射等方面的情况作一简要介绍．     

The influence from high-n dielectronic satellites to Kɑ resonance line in helium-like aluminium

Based on the multi-configuration Dirac-Fock method, this paper has made theoretical calculations for the dielectronic recombination cross-sections and the high-n dielectronic satellites to Kα resonance line in helium-like aluminium ions. It is found that high-n dielectronic satellites are seriously mixed with resonance line, which leads to a significant increase in both the apparent width and the intensity of Kα resonance line. They also induce a positional shift of Kα resonance line.     

人造卫星地面站基墩自振特性的原体试验

本文介绍了对几座人造卫星地面站天线基墩的自振特性在填土前后、有无翼肋及天线塔架安装前后等情况下进行的原体试验,结果表明,当基墩周围布置上十六根翼肋时,明显地增加了扭转和剪切刚度。