AEROENG 3521
Transcript Abbreviation:
Fnd Flt Veh Cntl
Course Description:
Linear dynamic systems analysis using Transfer function (Laplace Transformation based) methods and State Space (matrix theory based) methods with emphasis on aircraft and spacecraft models.
Course Levels:
Undergraduate (1000-5000 level)
Designation:
Required
General Education Course:
(N/A)
Cross-Listings:
(N/A)
Credit Hours (Minimum if “Range”selected):
3.00
Max Credit Hours:
(N/A)
Select if Repeatable:
Off
Maximum Repeatable Credits:
(N/A)
Total Completions Allowed:
(N/A)
Allow Multiple Enrollments in Term:
No
Course Length:
14 weeks (autumn or spring)
12 weeks (summer only)
Off Campus:
Never
Campus Location:
Columbus
Instruction Modes:
In Person (75-100% campus; 0-24% online)
Prerequisites and Co-requisites:
Prereq: 3520, and enrollment as AeroEng-BS student (No pre-majors can enroll in this class).
Electronically Enforced:
No
Exclusions:
(N/A)
Course Goals / Objectives:
Understanding and appreciation of common features of linear time-invariant (LTI) systems encountered in various engineering disciplines
Obtain the responses of LTI systems and quantify their performances both within open-loop and closed-loop environments
Cast various mechanical, aerospace, electrical and electro-mechanical systems into forms amenable to the methods they learn in this course
Identification of characteristic parameters of LTI's from the studies of experimental/test responses
Check if concurrence sought:
No
Contact Hours:
| Topic | LEC | REC | LAB | LAB Inst |
|---|---|---|---|---|
| Fundamentals of dynamic systems | 3.0 | 3.0 | 0.0 | 0 |
| Review of solution of differential equations by the Laplace transform methods | 6.0 | 6.0 | 0.0 | 0 |
| Block-Diagram Algebra | 3.0 | 3.0 | 0.0 | 0 |
| First -order Linear (LTI) systems Vehicle Simulations : Aircraft lateral and longitudinal dynamics simulations via transfer functions and MATLAB; Spacecraft attitude and rendezvous dynamics simulations via transfer functions and MATLAB | 6.0 | 6.0 | 0.0 | 0 |
| (LTI) Frequency-domain (Frequency Response) specifications. Connection between time domain and frequency domain, specifications and Bode plots. MATLAB Utility functions; Stability of LTI systems – Routh-Hurwitz criterion; Root Locus Technique | 6.0 | 6.0 | 0.0 | 0 |
| Multivariable (LTI) systems - State space (Time-domain) representation: The connection between state space and transfer function viewpoints , State-space Transition and Response by simulation; MATLAB Utility functions; | 3.0 | 3.0 | 0.0 | 0 |
| Vehicle Simulations : Aircraft lateral and longitudinal dynamics simulations via state-space and MATLAB; Spacecraft attitude and rendezvous dynamics simulations via state-space and MATLAB | 6.0 | 6.0 | 0.0 | 0 |
| Introduction to Digital systems: discrete difference equations, z-transform, sample and hold discrete sytems; block diagramming and open and closed-loop transfer functions, z-transform inversion, frequency domain in the z-plane. | 6.0 | 6.0 | 0.0 | 0 |
| Response to random inputs: Mean, variance, RMS, Fourier transform, Power spectral density, mean square response to random inputs, gust and launch responses, MATLAB utility functions | 3.0 | 3.0 | 0.0 | 0 |
| Total | 42 | 42 | 0 | 0 |
Grading Plan:
Letter Grade
Course Components:
Lecture
Recitation
Grade Roster Component:
Lecture
Credit by Exam (EM):
No
Grades Breakdown:
| Aspect | Percent |
|---|---|
| Homework | 20% |
| Midterm exams (2) | 50% |
| Final exam | 30% |
Representative Textbooks and Other Course Materials:
| Title | Author | Year |
|---|---|---|
| No Textbooks and Other Course Materials Entered. | ||
ABET-CAC Criterion 3 Outcomes:
(N/A)
ABET-ETAC Criterion 3 Outcomes:
(N/A)
ABET-EAC Criterion 3 Outcomes:
| Outcome | Contribution | Description |
|---|---|---|
| 1 | Substantial contribution (3-6 hours) | an ability to identify, formulate, and solve complex engineering problems by applying principles of engineering, science, and mathematics |
| 2 | Some contribution (1-2 hours) | an ability to apply engineering design to produce solutions that meet specified needs with consideration of public health, safety, and welfare, as well as global, cultural, social, environmental, and economic factors |
| 4 | Some contribution (1-2 hours) | an ability to recognize ethical and professional responsibilities in engineering situations and make informed judgments, which must consider the impact of engineering solutions in global, economic, environmental, and societal contexts |
| 6 | Some contribution (1-2 hours) | an ability to develop and conduct appropriate experimentation, analyze and interpret data, and use engineering judgment to draw conclusions |
| 7 | Some contribution (1-2 hours) | an ability to acquire and apply new knowledge as needed, using appropriate learning strategies |
Embedded Literacies Info:
Attachments:
(N/A)
Additional Notes or Comments:
(N/A)
Basic Course Overview:
AEROENG_3521_basic.pdf
(10.93 KB)