Background An icbm with a range of 6500 miles has a stagnation temperature of 12,000%F, 2000 f hotter than the surface of the sun Calculations showed that the optimum design for structural strength, resistance to heating, and free flight stability was a long, needle nosed reentry body But it would vaporize during reentry

The telemetry, tracking and control subsystem provides vital communication to and from the spacecraft TT&c is the only way to observe and to control the spacecraft's functions and condition from the ground October 29 2003 Massachusetts Institute of Technology

Autonomy Technologies Fault Detection, Isolation and Recovery Planning & Scheduling Intelligent Data Understanding Path Planning Gradient method

Why Cost Estimation? Critically important part of system design Too high- lose the contract award Too low-over-run cost plus contracts, company loss on fixed price contracts Trends Design to cost Cost as an independent variable

Deployment and Geometry Maintenance Deployable Membranes Used for solar arrays, sunshields, decoys Being researched for apertures starting at RF and eventually going to optical Inflatables First US satellite was inflated (ECHO D) Enables a very large deployment ratio -=deployed over stowed dimension

一、填空题(每空1分,共30分) 1、GPS由(空间星座)部分、()部分和()等三部分构。 2、开普勒六参数有s、()、()、()、()和（)。 3、电离层折射的影响白天比晚上(),冬天比夏天();卫星的

一、填空题(每空1分,共30分) 1、GPS由(空间星座)部分、()部分和( )等三部分构 2、开普勒六参数有s、()、()、()、()和() 3、电离层折射的影响白天比晚上(),冬天比夏天();卫星的

第一节电磁波传播的基本知识 电磁波及其参数,电磁波的波普。 第二节大气层对电磁波传播的概念 大气的结构及性质;对流层的影响及改正;电离层的影响及改正

第一节GPS定位的方法及观测量 定位方法的分类(动态与静态定位,绝对与相对定位,差分定位),观测量的基本 念(码相位观测量、载波相位观测量)。 第二节测码伪距观测方程与测相伪距观测方程 测码伪距观测方程及线性化;卫星载波信号的相位与传播时间,整周模糊度的概念, 测相伪距观测方程及线性化

第一节GPS定位的方法及观测量 定位方法的分类,观测量的基本概念。 第二节测码伪距观测方程与测相伪距观测方程 测码伪距观测方程;卫星载波信号的相位与传播时间,整周模糊度的概念,测相伪距观测方程