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NASA NTRS · 19750043414

Four-body trajectory optimization

Abstract

The two methods which are suitable for use in a 4-body trajectory optimization program are both multiconic methods. They include an approach due to Wilson (1970) and to Byrnes and Hooper (1970) and a procedure developed by Stumpff and Weiss (1968). The various steps in a trajectory optimization program are discussed, giving attention to variable step integration, the correction of errors by quadrature formulas, questions of two-impulse transfer, three-impulse transfer, and two examples which illustrate the implementation of the computational approaches.

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BibTeXRIS

Pu, C. L., Edelbaum, T. N.. 1975-03-01. Four-body trajectory optimization. https://ntrs.nasa.gov/citations/19750043414

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