Optimal low-thrust maneuvers near the libration points

Details Optimal low-thrust maneuvers near the libration points Optimal low-thrust maneuvers near the libration points

Dec 1980

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980jgc.....3..596m&link_type=abstract

Journal of Guidance and Control, vol. 3, Nov.-Dec. 1980, p. 596-598.

Physics

Earth-Moon System, Flight Optimization, Librational Motion, Low Thrust Propulsion, Spacecraft Maneuvers, Acceleration (Physics), Coriolis Effect, Differential Equations, Fuel Consumption, Variational Principles

Scientific paper

This paper is an extension of an investigation of the minimum propellant optimal maneuvers near the libration points in the earth-moon system. The previous study dealt exclusively with collinear libration points on the basis of some approximate solutions of the differential equations of the extremals (omega = 0). The study is completed with rigorous solutions both for collinear and equidistant libration points (omega not = 0). The influence of the components of the Coriolis acceleration which is neglected in the previous study is shown to be substantial.

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