3.1基本元件的承力特性 尽管一架飞机的机体是由成千上万个零 件组成,其构造相当复杂,但仍然可以认为 它是由一些最基本的元构件组成的

2.1飞机结构上的主要载荷 2.2不同飞行条件下的过载 2.3其它载荷情况 2.4疲劳载荷 2.5飞机设计规范简介

一、本课程的特点 注重基础理论概念的实用化、感性化以及工程化注重综合运用知识概念权衡复杂问题分析,抓住主要矛盾寻找解决问题途径的基本设计理念大量工程结构实例的剖析注重培养自行分析、动手设计的主观能力以及工程实用化的实践能力

6.1机身的功用、对机身的要求和机身的外形参数 构成、要求、分析设计方法与机翼基本相同 特殊性: 使用要求在设计中占有重要地位,对结构布置影响较大

Process Control plants 16.422 Continuous or batch processing Examples: Electricity generation(nuclear power plants), refineries, steel production, paper mills, pasteurization of milk Characterized by Large scale, both physically and conceptually Complex

Advantages of automation 16.422 · Improve efficiency productivity Task performance reliability Human safety both operators public Remote operations Reduction of human labor Technological advancements Improved quality of lif

The Coming Transition in Automobile Cockpits Insights from Aerospace Prof r, John Hansman Department of Aeronautics Astronautics

Consider Sensor System Display Or Threshold Sensor System Alert Radar Engine fire Detection

MERS Model-based programming of Cooperating explorers Brian c. williams CSAIL Dept. Aeronautics and astronautics Massachusetts Institute of Technology

Missions- Motivation Intelligence Reconnaissance Target Monitoring Forward air control E| ectronic Warfare a Search and rescue a Battle Damage Assessment BDA)