AE 508 Catalog 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;
second-order necessary and sufficient conditions for optimal
control problems.
Prerequisite: credit or concurrent
registration in AE 504.
4 hours.
Topics:
Orbital maneuvers and rocket dynamics
Review of Optimal Control Theory
Cost functionals for optimal trajectories
First-order necessary conditions for optimal low-thrust (continuous) trajectories
The primer vector and aspects of linear system theory
Necessary condition for optimal high-thrust (impulsive) trajectories
Optimal trajectories in linearized gravitational fields
Maximum number of impulses and sufficient conditions for linear problems
Cooperative rendezvous
Second-order necessary
conditions and sufficient conditions for optimal control problems