Spacecraft Dynamics and Control

University of Alabama

CourseAEM 425

Formulate, understand, and apply rigid body dynamics to a spacecraft. Determine the orientation of the spacecraft. Demonstrate the ability stabilize a spacecraft (gravity gradient, momentum-bias, spin stabilization). Perform analytic and numerical analysis to understand its behavior.

Credits

3 credits

Course Code

AEM 425

Related Courses

Prerequisites, corequisites, and courses that build on this one