1
课程详述
COURSE SPECIFICATION
以下课程信息可能根据实际授课需要或在课程检讨之后产生变动。如对课程有任何疑问，请联
系授课教师。
The course information as follows may be subject to change, either during the session because of unforeseen
circumstances, or following review of the course at the end of the session. Queries about the course should be
directed to the course instructor.
1.
课程名称 Course Title
航空飞行器动力学 Aircraft Flight Dynamics
2.
授课院系
Originating Department
力学与航空航天工程系 Department of Mechanics and Aerospace Engineering
3.
课程编号
Course Code
MAE312
4.
课程学分 Credit Value
3
5.
课程类别
Course Type
专业选修课 Major Elective Courses
6.
授课学期
Semester
秋季 Fall
7.
授课语言
Teaching Language
英文 English
8.
授课教师、所属学系、联系方
式（如属团队授课，请列明其
他授课教师）
Instructor(s), Affiliation&
Contact
（For team teaching, please list
all instructors）
王浩 研究助理教授
力学与航空航天工程系
wangh7@sustech.edu.cn
Wang Hao Research Assistant Professor
Department of Mechanics and Aerospace Engineering
wangh7@sustech.edu.cn
9.
实验员/助教、所属学系、联系
方式
Tutor/TA(s), Contact
待公布 To be announced
10.
选课人数限额(可不填)
Maximum Enrolment
（Optional）
授课方式
Delivery Method
讲授
Lectures
习题/辅导/讨论
Tutorials
实验/实习
Lab/Practical
其它(请具体注明)
Other（Please specify）
总学时
Total
11.
学时数
Credit Hours
48
48
2
12.
先修课程、其它学习要求
Pre-requisites or Other
Academic Requirements
高等数学（下）A 或者 数学分析 II 或者 高等数学（下）
Calculus II A or Mathematical Analysis II or Calculus II
13.
后续课程、其它学习规划
Courses for which this course
is a pre-requisite
无 NA
14.
其它要求修读本课程的学系
Cross-listing Dept.
无 NA
教学大纲及教学日历 SYLLABUS
15.
教学目标 Course Objectives
航空器飞行动力学是航空航天系本科生的专业选修课。 它在培养学生掌握飞行性能，飞行器平衡稳定性以及飞行控制方面
的分析和设计能力，以及在飞行器总体设计占据重要地位。
此课程将采用理清概念，理论分析，数值计算以及紧密联系现有无人机项目的方式实现课程目标。
航空器飞行动力学基本内容包括飞行性能，飞行器平衡稳定性以及飞行控制。
Aircraft flight dynamics is a major elective course for undergraduates in aerospace engineering. This course is important
for students in the aspects of understanding flight performance, stability, flight control and design.
In this course, theory, concepts and practice will be closely related to achieve course objectives. The basic contents
include aircraft flight performance analysis, equilibrium and stability, and feedback flight control.
16.
预达学习成果 Learning Outcomes
航空飞行动力学在飞行器性能分析和设计方面有着重要应用。通过此课程，学生能够全面掌握航空器飞行性能的分析与计
算方法，线性与非线性飞行器平衡稳定性的分析方法，以及了解飞行器主动控制的基本原理，能够在现有的开源飞控的基
础上，编纂自定义的飞控代码。这对于后续的飞行器整体设计具有重要意义。
Aircraft flight dynamics has practical application in aircraft flight performance analysis and design. After this course,
students are expected to fully understand the methodology of analyzing the flight performance of a given aircraft. The
second part is to know how to employ linear and non-linear flight stability analysis approaches in aircraft design.
Students are also expected to gain the skills of writing basic flight control codes. These outcomes will be further
implemented in the aircraft design course.
17.
课程内容及教学日历 （如授课语言以英文为主，则课程内容介绍可以用英文；如团队教学或模块教学，教学日历须注明
主讲人）
Course Contents (in Parts/Chapters/Sections/Weeks. Please notify name of instructor for course section(s), if
this is a team teaching or module course.)
3
Section 1
Introduction on aircraft flight dynamics （3 credit hours）
Section 2
Basic aircraft aerodynamics and propulsion characteristics（3 credit hours）
Section 3
Take-off and landing flight performance + Tutorial 1（3 credit hours）
Section 4
Climbing, gliding and turning flight performance （3 credit hours）
Section 5
Cruise flight performance -1（3 credit hours）
Section 6
Cruise flight performance -2 + Tutorial 2（3 credit hours）
Section 7
General equations of motion for Rigid body dynamics and linearization（ 3 credit
hours）
Section 8
Static stability and control devices-1 （3 credit hours）
Section 9
Static stability and control devices-2 + Tutorial 3（3 credit hours）
Section 10
Linear stability analysis in longitudinal motion （3 credit hours）
Section 11
Linear stability analysis in lateral-directional motion （3 credit hours）
Section 12
Nonlinear flight dynamic + Tutorial 4（3 credit hours）
Section 13
Introduction of basic feedback control and PID controller（3 credit hours）
Section 14
Basic flight control design （3 credit hours）
Section 15
More complicated topics in aircraft flight dynamics + Tutorial 5（3 credit hours）
Section 16
Revision and Final Exam （3 credit hours）
18.
教材及其它参考资料 Textbook and Supplementary Readings
教材：
1. Anderson, J. (1999). Aircraft performance and design, McGraw-Hill.
2. Nelson, R. C. (1998). Flight stability and automatic control, WCB/McGraw Hill.
参考书目：
1. Anderson, J. (2010). Fundamentals of Aerodynamics, McGraw-Hill.
2. R. F. Stengel, Flight Dynamics, Princeton University Press, 2004.
3. Etkin, B. and L. D. Reid (1995). Dynamics of Flight: Stability and Control, Wiley.
4. Wang, H (2016). Aerodynamics, Flight dynamics and Design of Wing-In-Ground (WIG) craft, Phd
Thesis.
课程评估 ASSESSMENT
19.
评估形式
Type of
Assessment
评估时间
Time
占考试总成绩百分比
% of final
score
违纪处罚
Penalty
备注
Notes
出勤 Attendance
4
课堂表现
Class
Performance
小测验
Quiz
20
课程项目 Projects
50
抄袭本项记 0 分
Cheating:0
平时作业
Assignments
期中考试
Mid-Term Test
期末考试
Final Exam
30
考试作弊本门课
程记 0 分
Cheating:0
期末报告
Final
Presentation
其它（可根据需要
改写以上评估方
式）
Others (The
above may be
modified as
necessary)
20.
记分方式 GRADING SYSTEM
A. 十三级等级制 Letter Grading
B. 二级记分制（通过/不通过） Pass/Fail Grading
课程审批 REVIEW AND APPROVAL
21.
本课程设置已经过以下责任人/委员会审议通过
This Course has been approved by the following person or committee of authority
力学与航空航天工程系教学指导委员会
The commission of teaching instruction in department of mechanics and aerospace engineering
