AE 403
Spring 2006 All Classes
All Classes
Credit: 3 OR 4 hours.
Theory and applications of spacecraft attitude dynamics and control; Euler angles, direction cosines, quaternions, and Gibbs-Rodrigues parameters; attitude sensors and control actuators; spin, three-axis active, reaction wheel, control moment gyro, and gravity gradient control systems; environmental effects.
3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: AE 352 and AE 353; or equivalents.
Section Status updates every 10 minutes.
| CRN | Type | Section | Time | Day | Location | Instructor | Section Details | |
|---|---|---|---|---|---|---|---|---|
|
29973
|
Lecture-Discussion
|
A
|
12:30PM
-1:50PM
|
TR
|
Talbot Laboratory
|
Prussing, J
|
|