A Modification of the Method of Transporting Trajectory

Details A Modification of the Method of Transporting Trajectory A Modification of the Method of Transporting Trajectory

Jan 2004

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2004cosre..42..103s&link_type=abstract

Cosmic Research, v. 42, Issue 1, p. 103-108 (2004).

Physics

Scientific paper

Further development of an approximate method for optimizing a flight with an ideally controlled small thrust is proposed. The method is based on the employment of the transporting trajectory and considered in [1-3]. A detailed analysis of the means of improving the accuracy of this method suggested in [2, 3] is carried out, and the solution is presented in finite form. The proposed approach is applied to the flights making flybys of many celestial bodies. In the case of small bodies the solution is also obtained in finite form. A numerical example is considered confirming the high efficiency of this method.

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