MAE 3307

SPACECRAFT DYNAMICS AND CONTROL.

University of Texas at Arlington · UGRD · Fall 2026

1 section

Catalog description

Fundamental principles and techniques of spacecraft rigid-body dynamics and control. Spacecraft attitude analysis using Euler angles and quaternions. Attitude disturbance torques, attitude determination methods, and basic concepts in feedback control, stability analysis, and hardware used in spacecraft attitude subsystem design. Modeling and simulation are key components in this course. Prerequisite: C or better in MAE 3304 .

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Class #texas_arlington_new-4186Fall 2026UGRD3 credits

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Instructor: Staff

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