NASA NTRS · 19690000667
Trajectory optimization using regularized variables
Abstract
Regularized equations for a particular optimal trajectory are compared with unregularized equations with respect to computational characteristics, using perturbation type numerical optimization. In the case of the three dimensional, low thrust, Earth-Jupiter rendezvous, the regularized equations yield a significant reduction in computer time.
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Lewallen, J. M., Szebehely, V., Tapley, B. D.. 1969-12-01. Trajectory optimization using regularized variables. https://ntrs.nasa.gov/citations/19690000667
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