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

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

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

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

Overview Autonomous Formation Flight: NASA RevCo Program Boeing is currently engaged with NASA Dryden Flight Research Center on a technically ambitious project, Autonomous Formation Flight(AFF). The projects primary goal is to investigate potential benefits of flying aircraft in the aerodynamic wake vortex emanating

5.1引言 5.2数字基带信号及其频谱特性 5.3基带传输的常用码性 5.4基带脉冲传输与码间干扰 5.5无码间干扰的基带传输特性 5.6眼图 5.7部分响应系统 5.8时域均衡

Prior to 767 somewhat arbitrary break at 100 seats DC-9 (2 person crew-pilot, co-pilot u B-727 3 person crew-pilot, co-pilot, flight engineer) B-757/767 Designed for 2 person Crew u Use of automation and simplified systems so minimize systems management u Use of advanced Cockpit to Increase Sa and make primary flight tasks

我们在上一讲中看到,很多系统的响应受某个特定模态的支配, 通常,对于航空航天系统,响应受到一对共轭复数极点的支配,利用 主导极点的概念,可以简化我们的设计问题,因为我们可以把注意力 集中在将这对主导极点配置在满意的位置上。注意,这就是我们用来 解决 Quansers问题的方法

Course objectives This is a graduate student class designed to examine the fundamental issues of human supervisory control, wherein humans interact with complex dynamic systems, mediated through various levels of automation this course will explore how humans interact with automated systems of varying complexities, what decision