Aircraft Dynamics First note that it is possible to develop a very good approximation of a key motion of an aircraft(called the Phugoid mode) using a very simple balance between the kinetic and potential energies Consider an aircraft in steady, level fight with speed Uo and height ho

Vice President/General Manager Engineering Military Aircraft and Missile Systems Group (retired), The Boeing Company Al Haggerty was vice president and general manager of Engineering for Boeing Military Aircraft and Missile System until March 31st, 2001. He was also the Executive Focal Point for the Lean Enterprise for the unit. Prior to this assignment, he was vice president of Engineering for

Handout 6: Proportional Compensation Eric Feron Feb25,2004 Plant under study: 1/10 G(s)=(s+1)(s/10+1)2 Compensation Scheme: We adjust the gain K in the feedback loop (draw the feedback loop below)

Handout 7: Lag and PI compensation Eric Feron Lag Compensation goals: Raise gain at low frequencies while leaving rossover &z higher frequencies untouched b≥0. When b=0: Add an integrator in the loop Typical lag Bode Plot

Handout 4: Root-Locus Review Eric Feron Feb17,2004 Summary of Guidelines for plotting a root-locus 1. Mark Poles X and Zeros O 2. Draw the locus on the real axis to the left of an odd number of real poles plus zeros

Handout 2: Gain and Phase margins Eric Feron Feb6,2004 Nyquist plots and Cauchy's principle Let H(s) be a transfer function. eg H(s)= s2+s+1 (s+1)(s+3) Evaluate H on a contour in the s-plane. (your plots here)

本章的目的是为了使航空专业的学生能熟悉飞机设计过程中所用的设计决策方法,了解飞机设 计的任务来源与如何进行最初阶段的设计工作。“初始总体参数的确定”和“方案设计”这两个词 表示的便是这一阶段的设计。初始设计阶段之后的情况很大程度上取决于初始设计阶段的结果和研 制成本

本书是航空高等院校飞行器设计专业本科生 的必修课教材,重点讲述了飞机总体设计的 基本原理和方法。强调飞机总体设计的综合 协调、折衷权衡、反复迭代等特点,通过几 个循环,由简到繁完成飞机的总体设计,锻 炼增强学生的综合分析和决策问题的能力

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