AME454
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AME454 - Spacecraft Attitude Dynamics and Control
Course Description
Spacecraft attitude description on SO(3) using rotation matrices and attitude parameterizations; Wahba's problem and static attitude determination; rigid body dynamics, torque-free attitude dynamics and stability of rigid body motion; gravity gradient torque and stabilization, nutation damping, reaction control thrusters, and momentum exchange actuation; nonlinear regulator and attitude tracking using feedback control.
Min Units
3
Max Units
3
Repeatable for Credit
No
Grading Basis
GRD - Regular Grades A, B, C, D, E
Career
Undergraduate
Enrollment Requirements
016524
May be convened with
AME554
Name
Lecture
Workload Hours
3
Optional Component
No
Typically Offered Main Campus
Spring