Method for solving a two-point boundary value problem of the optimization of low-thrust transfer trajectories

Details Method for solving a two-point boundary value problem of the optimization of low-thrust transfer trajectories Method for solving a two-point boundary value problem of the optimization of low-thrust transfer trajectories

Nov 1984

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1984kosis..22..842g&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 22, Nov.-Dec. 1984, p. 842-847. In Russian.

Physics

Boundary Value Problems, Low Thrust Propulsion, Spacecraft Trajectories, Trajectory Optimization, Transfer Orbits, Comets, Gravitational Fields, Integral Equations, Vector Analysis

Scientific paper

A 'pulse-spreading' (PS) method is proposed for obtaining the initial approximation for optimal jet-powered acceleration in calculations of the low-thrust transfer trajectories of spacecraft in a central gravitational field. The PS method is shown to be superior to existing methods (particularly the 'transporting-trajectory' method) for angular transfer distances of the order of 360 deg and large eccentricities of the initial and/or final orbits.

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