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Aug 16, 2024
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AE 245 - Spacecraft Dynamics and Control 3 units Rigid body dynamics review. Attitude kinematical representations. Development and solution of general equations of motion. Single and dual-spin, zero and biased-momentum spacecraft. Control system design strategies. Common torquer elements. Computer simulations.
Prerequisite(s): BSAE or Instructor Consent. Grading: Graded
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