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Full-state Feedback Control How do we change the poles of the state-space system? Or, even if we can change the pole locations Where do we put the poles? Linear Quadratic Regulator Symmetric Root Locus How well does this approach work? Copyright [2001 by JOnathan dHow
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Class expectations This is a graduate level class. There is no final exam Grading in the class is based on homework (75%) and on a final written report(25%) The report will be revised during semester and should be 2000-3000 words(8-10 double spaced pages)
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MG!∈R- ORDER5)sT6As RREL丹T(0sHP5 BETWEEN1MER6soN5毛 TAST∈P兵 ND THE POLE LOCAT(0NS心EK ALCULATE0 FoR A SECOND-ORDER SYSTEM GuES60工 NSIGHTS AcTuALLy Gooo APPRoXIMATIONS foR MAwy HIGHER- ORDER SYSTEMS BECAUSE THEIR
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Controllability Definition: An LTI system is controllable if, for every a*(t d every T>0, there exists an input function u(t),0
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In going from the state space model i(t)=A.(t)+ Bu(t y(t)= Ca(t)+ Du(t) to the transfer function G(s)=C(sI -A)-B+D need to form the inverse of the matrix(sI- A)-a symbolic inverse- not easy at all For simple cases, we can use the following
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5.4.1 CSCW系统的发展与分类 5.4.2 CSCW系统的概念特征 1. CSCW系统的技术特点 2. CSCW系统的工作模式 3. CSCW系统的时∕空划分模型 5.4.3 CSCW系统实现模型与方法 1. 群体协作模型 2. 基于Web的CSCW模型 3. 关键实现方法 4. 透明合作方法和有意识合作方法
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4.1引言 4.2幅度调制的原理及抗噪声性能 4.3角度调制的原理及抗噪声性能 4.4各种模拟调制系统的性能比较 4.5频分复用 4.6复合调制及多级调制的概念
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7-1 非线性问题概述 7-2 常见非线性因素对系统运动特性的影响 7-3 相平面法基础 7-4 非线性系统相轨迹分析 7-5 描述函数 7-6 用描述函数分析非线性系统
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4.1 操纵系统的特性 4.2 现代高速飞机稳定性和操纵性的基本特点与操纵系统设计 4.3 飞机主动控制技术 4.4 电传操纵系统 4.5 综合飞行控制系统
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Missy Cummings Mary( Missy) Cummings received her B.S. in Mathematics from the United States Naval Academy in 1988, her M.S. in Space Systems Engineering from the Naval postgraduate School in 1994, and her Ph. D in Systems Engineering from the University of Virginia in 2003. A naval officer and military pilot from
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