AOE 4140:

Spacecraft Dynamics and Control

Overview Space missions and the pointing requirements affect attitude control systems. Rotational kinematics and attitude determination algorithms. Modeling and analysis of the attitude dynamics of space vehicles. Rigid body dynamics, effects of energy dissipation. Gravity gradient, spin, and dual spin stabilization. Rotational maneuvers. Environmental torques. Impacts of attitude stabilization techniques on mission performance. AOE4134 and AOE3034 are prerequisites.
Class Time MWF 11:15am - 12:05pm
Location RAND 216
Office Hours MW 9:30-10:30 am, R 1:30-2:30pm (or by appointment)
Syllabus AOE 4140
Text Book H. Schaub and J. L. Junkins, Analytical Mechanics of Space Systems, AIAA Education Series, Reston, VA, 2003.