NASA NTRS · 19690060557
Coordinate system influence on the regularized trajectory optimization problem.
Abstract
Numerical integration for continuously thrusting spacecraft optimal trajectory, considering rectangular Cartesian and polar cylindrical coordinates characteristics
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Lewallen, J. M., Schwausch, O. A., Tapley, B. D.. 1969-08-01. Coordinate system influence on the regularized trajectory optimization problem.. https://ntrs.nasa.gov/citations/19690060557
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