ACCAD 5522

Intermediate Astronautics

Ohio State University-Mansfield Campus · UGRD · Fall 2026

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Intermediate orbital mechanics with coverage of advanced solution methods of the two-body problem, the two-body two-point boundary value problem, initial orbit determination and statistical orbit determination (IOD-OD), and foundations of non-Keplerian motion including the three-body problem and orbital perturbations. Prereq: AeroEng 3522 and MechEng 2030; or Grad standing in Engineering; or permission of instructor. Not open to students with credit for AeroEng 5626.

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Class #ohio_mansfield_campus-ACCAD5522Fall 2026UGRD3 credits
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