Mar 28, 2024  
2022-2023 Academic Catalog 
    
2022-2023 Academic Catalog [ARCHIVED CATALOG]

Add to Favorites (opens a new window)

AE 243 - Advanced Astrodynamics


3 unit(s)
Analysis of spacecraft motion using different dynamic models and perturbations. Use of the state transition matrix and differential corrections technique for trajectory computation. Orbit determination and station-keeping methods. Introduction to the three-body problem. Application of computational and analytic methods to solve astrodynamic problems.

Prerequisite(s): BS in Aerospace Engineering or instructor consent.
Grading: Letter Graded


Class Schedule | Syllabus Information | University Bookstore




Add to Favorites (opens a new window)