NASA NTRS · 19690039585
The Hamilton-Jacobi method applied to the low-thrust trajectory problem.
Abstract
Spacecraft optimum low thrust trajectory analyzed by Hamilton-Jacobi perturbation theory, obtaining canonic constants of motion
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Miner, W. E., Powers, W. F., Tapley, B. D.. 1968-01-01. The Hamilton-Jacobi method applied to the low-thrust trajectory problem.. https://ntrs.nasa.gov/citations/19690039585
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