1. Development of an Optimized Lambert Problem Solver for Targeting Elliptical Orbits Open Access Author: Shank, Brian Steven Title: Development of an Optimized Lambert Problem Solver for Targeting Elliptical Orbits Graduate Program: Aerospace Engineering Keywords: Lambert's ProblemPork Chop PlotATSVVisual Data TechniquesOrbital MechanicsAstrodynamicsMission PlanningPropulsion Optimization File: Download BrianShank_FinalThesis.pdf Committee Members: Dr David B Spencer, Thesis Advisor/Co-Advisor
2. Evolutionary Computation for Spacecraft Trajectory Optimization Open Access Author: Sottile, Brad Joseph Title: Evolutionary Computation for Spacecraft Trajectory Optimization Graduate Program: Aerospace Engineering Keywords: AstrodynamicsEvolutionary AlgorithmsEvolutionary ComputationEvolutionary StrategiesOptimizationSpacecraft Trajectory File: Download Sottile_-_Evolutionary_Computation_for_Spacecraft_Trajectory_Optimization.pdf Committee Members: Robert Graham Melton, Thesis Advisor/Co-Advisor