Linearization methods for optimizing the low thrust spacecraft trajectory: Theoretical aspects


Cite item

Full Text

Open Access Open Access
Restricted Access Access granted
Restricted Access Subscription Access

Abstract

The theoretical aspects of the modified linearization method, which makes it possible to solve a wide class of nonlinear problems on optimizing low-thrust spacecraft trajectories (V. V. Efanov et al., 2009; V. V. Khartov et al., 2010) are examined. The main modifications of the linearization method are connected with its refinement for optimizing the main dynamic systems and design parameters of the spacecraft.

About the authors

P. V. Kazmerchuk

Federal Enterprise “Lavochkin Association”

Author for correspondence.
Email: pavel.kazmerchuk@gmai.com
Russian Federation, Khimki, Moscow oblast

Supplementary files

Supplementary Files
Action
1. JATS XML

Copyright (c) 2016 Pleiades Publishing, Inc.