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Optimum Interplanetary Rendezvous Trajectories With Power-Limited Vehicles
Astrodynamics-optimization theory and guidance theory Research achievements review series no. 15-16
Rocket trajectory optimization final technical summary report, mar. 1961 - dec. 1964
Launch vehicle optimization, phase II. VOLUME I - Concept development and application Final report
Mission logic development and trajectory prediction, determination and optimization Final report
Optimization of Saturn IB and V mounting and thermal conditioning panels Final report
Optimization of hydraulic thrust vector control systems for launch vehicles, volume III, section 2
Applications of the calculus of variations to aircraft performance