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AE 403 - Spacecraft Attitude Control

Spring 2021

Official Description

Theory and applications of spacecraft attitude dynamics and control; Euler angles, direction cosines, quaternions, and Gibbs-Rodrigues parameters; attitude sensors and control actuators; spin, three-axis active, reaction wheel, control moment gyro, and gravity gradient control systems; environmental effects. Course Information: 3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: AE 352 and AE 353.

Related Faculty

Spacecraft Attitude ControlA29973LCD1530 - 1650 T R    Christian Miguel Chilan
Spacecraft Attitude ControlONL62470ONL -    Christian Miguel Chilan