|
Dec 07, 2024
|
|
|
|
AEE 4263 Space Flight MechanicsCredit Hours: 3 Provides understanding of the motion of celestial objects and spacecraft under gravity. Includes analysis of the two-body and restricted three-body problems and orbital transfer using impulsive forces. Also includes designing interplanetary spacecraft trajectories for given specifications. Uses MATLAB® for numerical analyses and dynamic simulation. Prerequisite: MEE 2082 and (MTH 2201 or MTH 3200 )
Add to Personal Catalog (opens a new window)
|
|