Approximate solutions of the Euler-Lambert equation for several revolutions about a central body

Details Approximate solutions of the Euler-Lambert equation for several revolutions about a central body Approximate solutions of the Euler-Lambert equation for several revolutions about a central body

Nov 1984

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1984kosis..22..942l&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 22, Nov.-Dec. 1984, p. 942-944. In Russian.

Physics

Euler-Lambert Equation, Interplanetary Trajectories, Orbit Calculation, Trajectory Optimization, Approximation, Fuel Consumption, Mars (Planet), Venus (Planet)

Scientific paper

Approximate solutions are obtained for the Euler-Lambert equation with
the aim of economizing machine time in the framework of designing
fuel-optimal spacecraft trajectories. The results, obtained for several
revolutions about a central body, are applicable to the
earth-Venus-earth and earth-Mars-earth trajectories.

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