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Solar System Research

, Volume 52, Issue 7, pp 630–635 | Cite as

Linearization Methods for Problems of Optimizing Low-Thrust Spacecraft Trajectories: Verification Procedure

  • P. V. KazmerchukEmail author
Article
  • 5 Downloads

Abstract

Several well-studied problems for optimizing low-thrust spacecraft trajectories are solved using the modified linearization method (MLM). The results are compared with the results obtained by other authors. On this basis, conclusions are drawn on the possible use of the modified linearization method for optimizing low-thrust spacecraft trajectories.

Keywords

linearization method low thrust nonlinear optimization 

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Copyright information

© Pleiades Publishing, Inc. 2018

Authors and Affiliations

  1. 1.Lavochkin AssociationKhimki, Moscow oblastRussia

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