多载波DS—CDMA在数字微波通信系统中的应用

基于数字微波通信系统的特点，介绍了多载波SD-CDMA（Multicarrier-DS-CDMA,即MC-DS-CDMA）调制技术的基本原理及其应用于数字微波通信系统中的具体实现方法。从理论上详细地分析了MC-CDMA工作方式的性能，并将其与传统的数字微波通信系统进行了比较，阐明了将MC-DS-CDMA工作方式应用于数字微波通信系统的必要性。     

混沌测控的概念、特性与实现

概述了混沌测控的基本概念，归纳了混沌序列的主要特性并与m、Gold序列进行了比较，介绍了混沌序列的种类和截断码的码库生成，提出了截断混沌序列和无限混沌序列的测控通信系统方案设想。     

海事BGAN系统数据链路测试及性能分析

概述了海事第4代卫星及BGAN系统的基本情况,针对某特殊用户对BGAN系统提出的要求,在数据Standard IP型和信道Streaming IP型2种通信业务模式下,对通信网络链路的时延、抖动、丢帧等性能进行测试实验,分析测试结果,证实了BGAN系统在远洋船舶中使用的可行性。     

Inflatable antenna for cubesats: Motivation for development and antenna design

CubeSats and small satellites have potential to provide means to explore space and to perform science in a more affordable way. As the goals for these spacecraft become more ambitious in space exploration, moving from Low Earth Orbit (LEO) to Geostationary Earth Orbit (GEO) or further, the communication systems currently implemented will not be able to support those missions. One of the bottlenecks in small spacecraft communication systems is represented by antennas' size, due to the close relation between antenna gain and dimensions. Current antennas for CubeSats are mostly dipole or patch antennas with limited gain. Deployable (not inflatable) antennas for CubeSats are currently being investigated, but these solutions are affected by the challenge of packaging the whole deployable structure in a small spacecraft.The work that we propose represents the first attempt to develop an inflatable antenna for CubeSats. Inflatable structures and antennas can be packaged efficiently occupying a small amount of space, and they can provide, once deployed, large dish dimension and correspondent gain. Inflatable antennas have been previously tested in space (Inflatable Antenna Experiment, STS-77). However they have never been developed for small spacecraft such as CubeSats, where the packaging efficiency, the deployment, and the inflation represent a challenge.Our study explores for the first time the possibility of developing such antenna in a way compatible with CubeSat dimensions and constraints. The research provides answers on the possible dimensions for an inflatable antenna for small satellites, on the gain and resolution that can be achieved, and on the deployment and inflation mechanism compatible with CubeSat. Future work in the development of the antenna will include the test of the antenna in flight during a specific technical demonstration mission.The article is structured as follows: context and motivation for Cubesat inflatable antenna are described; then a study to design the antenna which achieves the required performance metrics, while respecting the constraints imposed by CubeSat structure, is presented.     

STW试验通讯卫星远地点发动机真空总冲测试技术

本文介绍了影响STW试验通讯卫星固体推进剂远地点发动机真空冲测量的各种因素及其所造成的不确定度大小,着重介绍了推力、燃烧室压强、负压等参数的误差源.总结了该发动机高空模拟试车的经验,同时叙述了降低真空总冲测量不确定度的设想与实现途径.     

电缆充气机控制系统的设计

本文较详细的介绍电缆自动充气机控制系统的组成及工作原理，重点论述压力、湿度传感器的调理电路，并给出系统工作的主程序。     

在VAX／VMS系统上实现进程间的同步,通信和共享的几种方法

在卫星数据的实时传输及数据的并行处理应用中,对进程的同步、通信和共享都有很高的要求,象响应时间,数据的完整性等等。本文结合作者在工作中使用的方法,讨论了在VAX/VMS 系统上实现进程间同步、通信及共享的几种方法。     

通信卫星的热控制技术

本文扼要地介绍了通信卫星热控技术的现状和近期的发展前景,并对辐射器及其它热控措施的若干问题进行具体讨论。     

我国Ku波段广播通信卫星赋形波束天线设计

讨论了我国Ku 波段广播通信卫星全国覆盖的赋形波束天线的设计问题。就我国目前的技术和工艺水平,提出了三种可行的方案;通过这三种方案,介绍了偏馈反射面天线的几何尺寸的选择,多波束天线的馈源位置排列及缋源幅相激励系数的优化步骤;最后绘制了三种方案的等值线覆盖图,分析和比较了它们各自的优缺点。     

LEO卫星网中MPLS协议体系及其实现方案

由于卫星网拓扑时变的特性,使得现有的多协议标签交换(MPLS)技术难以在卫星网中有效地运行。以铱(Irid ium)系统为例,首先分析低轨卫星网(LEO)中星际链路的变化情况。针对卫星网具有频繁断接性和传输大时延等特点,将基于MPLS技术的LEO卫星网系统进行功能模块的划分,并重点对MPLS协议中的标签设计、信令协议选择、标签交换路径(LSP)的切换等问题进行仿真,同时提出相应的改进方案。