AEM 425 - Spacecraft Attitude Dynamics and Control

Institution:

The University of Alabama

Subject:

AEM-Aerospace Engr & Mechanics

Description:

3 hours. Prerequisite: AEM 468. This course introduces the student to the theory and practice of spacecraft dynamics and control. The topics covered include kinematics and dynamics of angular motion, spacecraft stabilization, attitude control devices, and design of linear and nonlinear spacecraft control systems.

Credits:

0.00 - 3.00

Credit Hours:

Prerequisites:

Corequisites:

Exclusions:

Level:

Instructional Type:

Lecture

Notes:

Additional Information:

Historical Version(s):

Institution Website:

www.ua.edu/

Phone Number:

(205) 348-6010

Regional Accreditation:

Southern Association of Colleges and Schools

Calendar System:

Semester

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