AERO 650
Spacecraft Attitude Determination
Texas A&M University · UGRD · Fall 2026
1 section
Catalog description
Credits 3. 3 Lecture Hours. Spacecraft attitude determination systems; attitude and error parameterizations, attitude sensors, data processing and calibration; introduction to single- and three- axis attitude determination and to optimal attitude and error estimation: ECI motion and time definitions. Prerequisite: AERO 423 or equivalent.
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Availability not recently verifiedClass #texas_am-0215Fall 2026UGRD
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