| 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. |