Course Websites

AE 508 - Optimal Space Trajectories

Last offered Spring 2024

Official Description

Optimal rocket trajectories in inverse-square and linearized gravitational fields; orbital transfer, intercept, and rendezvous; high-thrust (impulsive) and low-thrust (continuous) trajectories; primer vector theory and applications; cooperative rendezvous. Course Information: Prerequisite: Credit or concurrent registration in AE 504.

Related Faculty

Optimal Space TrajectoriesA30029LCD41100 - 1220 M W  1302 Siebel Center for Comp Sci Robyn Woollands