AE 508
spring 2014
All Classes
Optimal Space Trajectories
Credit: 4 hours.
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.
Prerequisite: Credit or concurrent registration in AE 504.
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