AE 426 - Spacecraft Attitude Dynamics

Institution:

Embry-Riddle Aeronautical University-Daytona Beach

Subject:

Description:

Fundamentals of spacecraft attitude dynamics. Three-dimensional rigid-body kinematics. Stability and dynamics of symmetric and tri-inertial bodies. Attitude, nutation, and spin-control maneuvers for spin-stabilized spacecraft. Effects of energy dissipation. Momentum-biased spacecraft dynamics. Stability, modeling, and simulation of spin-stabilized and momentum-biased spacecraft. Elements of threeaxis stabilized spacecraft. Effects of gravity gradient, solar radiation pressure, atmospheric drag, and magnetic torque on spacecraft attitude. Prerequisites: AE 313, MA 345.

Credits:

3.00

Credit Hours:

Prerequisites:

Corequisites:

Exclusions:

Level:

Instructional Type:

Lecture

Notes:

Additional Information:

Historical Version(s):

Institution Website:

www.erau.edu

Phone Number:

(800) 222-3728

Regional Accreditation:

Southern Association of Colleges and Schools

Calendar System:

Semester

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