ASEN 5010:

Spacecraft Dynamics and Control

Overview Studies the rotational motion of spacecrafts, including attitude parameters and spacecraft torques. Applies Euler equations to the attitude motions of simple spacecrafts and their stability. Pre: ASEN 3200 or equivalent, or permission of instructor. (3H, 3C)
Class Time TR 12:30-1:45am
Location ECCS 1B12
Office Hours M 2:30-4:00pm, W 9:00-10:00am (or by appointment)
Syllabus ASEN 5010
Text Book H. Schaub and J. L. Junkins, Analytical Mechanics of Space Systems, AIAA Education Series, 3rd Edition, Reston, VA, 2014.