一、岩浆岩体的产状及其构造控制 二、岩浆岩体的原生构造 三、岩浆岩体的次生构造 四、岩浆岩体构造的观察和研究

计算机的应用已不再局限于科学计算,而更多地用 于控制、管理及数据处理等非数值计算的处理工作 与此对应,计算机加工处理的对象由纯粹的数值发 展到字符、表格和图像等各种具有一定结构的数据 为了编写出一个“好”的程序,必须分析待处理的对 象的特征以及各对象之间存在的关系,这就是“数 据结构”这门学科形成和发展的背景

5.1 使用AWT(Abstract Window Toolkit)构件 5.2 包含构件的构件----构件容器（container） 5.3 事件的传递 5.4 各种构件的应用实例(一) 5.5 外观的管理与控制 5.6 各种构件的应用实例(二) 5.7 总结

SYSTEM TDENTIFICATION DEVELOPING AN APPR0 PR1ATE MOOEL OF A YWAMIC SYSTEM US(NG BSERVED DATA COMBINEO WITH: BASIC MECHANICS AND OYNAMICS PR1OR KNOWLEVGE oF RELATIONSKIPS BETWEEN SIGNALS INPUT/OUTPUT MOOELS

Bachelor of Engineering The State University of Buffalo, 2002 Submitted to the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics and Astronautics

Lateral Autopilots We can stabilize/modify the lateral dynamics using a variety of dif- ferent feedback architectures

INERTIAL SENSoRS MoST, IF NoT ALL, INETIAL SEN SORS MEASURE RATES LINE4R R ANGULAR) 6R ACCELERATIONS WHILE THE RATE INFORMATION IS TYPLCALLY VALIO VER LONG PERIODS of TIME) IT MUST BE INTEGRATED To CET

Complementary Filter(CF) Often, there are cases where you have two different measurement sources for estimating one variable and the noise properties of the two measurements are such that one source gives good information only in low frequency region while the other is good only in high frequency region

Goal: analyze aircraft longitudinal dynamics to determine if the be- havior is acceptable, and if not, then modify it using feed back control Note that we could (and will)work with the full dynamics model but for now, let's focus on the short period approximate model from

State Space Basics State space models are of the form x()= Ax(t)+ Bult) y(t)= Cx(t)+ Dult) with associated transfer function G()=C(sI-A)