AEROENG 5621
Transcript Abbreviation:
S/C Control
Course Description:
Spacecraft (satellite) control systems analysis and design.
Course Levels:
Undergraduate (1000-5000 level)
Graduate (5000-8000 level)
Designation:
Elective
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: 3521 (521).
Electronically Enforced:
No
Exclusions:
Not open to students with credit for 620 or 621.
Course Goals / Objectives:
(N/A)
Check if concurrence sought:
No
Contact Hours:
| Topic | LEC | REC out-of-class | REC in-class | Weekly LAB out-of-class | Weekly LAB in-class |
|---|---|---|---|---|---|
| Review of Equations of Motion for Orbit Dynamics and Spacecraft (Satellite) Attitude dynamics in Principal Axes frame | 0.0 | 0.0 | 0 | 0.0 | 0 |
| Single and Dual Spin Stabilization; Active Nutation Control; Despinning and Denutation of a satellite; Active Momentum bias stabilization | 0.0 | 0.0 | 0 | 0.0 | 0 |
| Gravity Gradient Stabilization with passive and active damping; with three axis magnetic active damping | 0.0 | 0.0 | 0 | 0.0 | 0 |
| Momentum Wheel (Reaction Wheel) based Active Three axis attitude control systems | 0.0 | 0.0 | 0 | 0.0 | 0 |
| Reaction Jet based Active Three axis Attitude Control Systems; Combination of these with various types of measurements | 0.0 | 0.0 | 0 | 0.0 | 0 |
| Attitude maneuvers in Space; Active Control using momentum exchange devices, magnetic torquers; Time optimal attitude control | 0.0 | 0.0 | 0 | 0.0 | 0 |
| Attitude Sensors and Orbit and Attitude control hardware. | 0.0 | 0.0 | 0 | 0.0 | 0 |
| Reentry Dynamics; Rocket/Missile gravity turn trajectories | 0.0 | 0.0 | 0 | 0.0 | 0 |
| Structural Flexibility Effects; Liquid Sloshing | 0.0 | 0.0 | 0 | 0.0 | 0 |
| Total | 0 | 0 | 0 | 0 | 0 |
Grading Plan:
Letter Grade
Course Components:
Lecture
Grade Roster Component:
Lecture
Credit by Exam (EM):
No
Grades Breakdown:
| Aspect | Percent |
|---|---|
| Homework | 15% |
| Midterm exams (2) | 50% |
| Final exam | 35% |
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:
| Substantial contribution (3-6 hours) | 1 | an ability to identify, formulate, and solve complex engineering problems by applying principles of engineering, science, and mathematics |
| Substantial contribution (3-6 hours) | 2 | 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 |
| Some contribution (1-2 hours) | 4 | 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 |
| Some contribution (1-2 hours) | 7 | an ability to acquire and apply new knowledge as needed, using appropriate learning strategies |
Embedded Literacies Info: