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Inter-orbital low-thrust transfers in an arbitrary field of forces

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Abstract

Low-thrust transfers between preset orbits are considered in the presence of perturbations of different origin. A simple method of finding the transfer trajectory is suggested, based on linearization of motion near reference orbits. The required accuracy of calculations is achieved by way of increasing the number of reference orbits. The method can also be used in the case of a large number of revolutions around the attracting center: no averaging of motion is required in this case. The suggested method is applicable as well, when the final orbit is specified partially and when there are constraints on the thrust direction. The optimal solution to the linearized problem is not optimal for the original problem; closeness of solutions to these two problems is estimated using a numerical example. Capabilities of the method are also illustrated by examples.

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Authors and Affiliations

  1. Space Research Institute, Russian Academy of Sciences, Profsoyuznaya ul. 84/32, Moscow, 117997, Russia

    A. A. Sukhanov

  2. National Institute of Space Research, Sao Jose dos Campus, Brazil

    A. F. B. de A. Prado

Authors
  1. A. A. Sukhanov
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  2. A. F. B. de A. Prado
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Correspondence to A. A. Sukhanov.

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Original Russian Text © A.A. Sukhanov, A.F.B. de A. Prado, 2013, published in Kosmicheskie Issledovaniya, 2013, Vol. 51, No. 2, pp. 159–175.

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Sukhanov, A.A., de A. Prado, A.F.B. Inter-orbital low-thrust transfers in an arbitrary field of forces. Cosmic Res 51, 147–163 (2013). https://doi.org/10.1134/S0010952513020056

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