AEM5431
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AEM 5431 - Trajectory Optimization (3 Cr.)
Course description
Parameter optimization problems. Calculus of variations. Nonlinear optimal control problems. Trajectory optimization algorithms. Steady-state aircraft flight. Minimum-time climb aircraft trajectory. Aero-assisted orbital transfer trajectories. Optimal space trajectories.prereq: 4321 or EE 4231 or ME 5281 or equiv
Minimum credits
3
Maximum credits
3
Is this course repeatable?
No
Grading basis
OPT - Student Option
Lecture
Requirements
013129
Fulfills the writing intensive requirement?
No
Typically offered term(s)
Periodic Fall & Spring