585. Spacecraft Attitude Determination and Control (3)
- Prerequisite: MAE 501 or equivalent. Rigid-body dynamics.
- Control systems. Spacecraft attitude dynamics and control. Stabilization methods and maneuvers. Impact of flexible structures.
- (Lecture-Problems 3 hours) Letter grading only (A-F).
Course Outline
Class Schedules
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Mechanical Engineering (MAE)
Engineering Technology (ET)
Engineering (ENGR)
Official Program Information
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year you enter(ed) the program.