Koofers

MAE 3304 - ASTRONAUTICS I at University of Texas - Arlington

Description:

Introduction to astronautics, the solar system, and the two-body problem. Orbit shaping and orbit transfers. Patched conic approximations for interplanetary transfers. Introduction to the three-body problem and relative motion. Rigid spacecraft equation of motion. Active and passive attitude stabilization techniques for spacecraft. Semesters offered: Fall. Prerequisite: C or better in MAE 2323,C or better in MAE 2360, C or better in MAE 3360.

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