Ideal response Want Ideal Response to Signal -usuall straight-line function Actual response is determined by values of control factors and noise factors If noise factors are suppressed early, the en difficult problems only appear late Introduce noises early C Don Clausing 1998

Comments on hw#2 and Quiz #1 Questions on the reading Quiz Brief lecture Paper Helicopter Experiment Robust System Design 16.881

Case study An automatic document handler(adh)was developed at the ss level. When integrated into the total system there were many new problems. The TQM Problem Solving Process was used, and many problems were solved. However. at the field readiness Test (frt) before entering production the reliability was 15X worse than acceptable O Don Clausing 1998

Background SDM split-summer format M Heavily front-loaded Systems perspective Concern with scaling Product development track, CIPD Place in wider context of product realization Joint 16(Aero/Astro)and 2(Mech E) Robust system design

1·飞行力学学科的定义 飞行力学学科的定义有不同的说法,最一般的说法是飞行力 学是研究飞行器运动规律的学科,是应用力学的一个新分支。它 是按照力学的基本原理结合具体对象一—飞行器来分析、研究在 有控制或无控制情况下飞行器运动特性的一门学科

Agenda DREAMLINER 5000 psi Hydraulics System Configuration Update Hydraulic Architecture System Interfaces Component Installations Landing Gear Actuation System Overview Landing Gear Actuation System Steering System Boeing Proprietary ABDEIND

航空安全（民航安全）：航空安全自愿报告系统

航空安全（民航安全）：民航安全管理 (基础篇)

民航学院：航空安全（民航安全）——民航安全管理基础篇

安全管理机构 ·民航安全法规体系 中国民航规模