Learning objectives Introduce explore orthogonality Study the standard oas Practice computing dOF of an experiment Learn how to select a standard oa Introduce means to modify Oas Consider studying interactions in Oas Robust System Design
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Failure modes Noises lead to failure modes(Fm) One set of noise values leads to fm Opposite set of noise values leads to FM Simple problem solving chases the problem from Fm, to Fm, and back again but does not avoid both fms with the same set of design values-endless cycles of build/test/fIx(B/T/F) C Don Clausing 1998 6.881
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Proposed Schedule Changes · Switch lecture No quiz Informal (ungraded) presentation of term project ideas Read Phadke ch. 7-- Construction Orthogonal Arrays -Quiz on ANOVA Noise experiment due Robust System Design
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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
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Comments on hw#2 and Quiz #1 Questions on the reading Quiz Brief lecture Paper Helicopter Experiment Robust System Design 16.881
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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
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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
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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
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