Email this article Linearization methods for optimizing the low thrust spacecraft trajectory: Theoretical aspects
- Authors: Kazmerchuk P.V.1
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Affiliations:
- Federal Enterprise “Lavochkin Association”
- Issue: Vol 50, No 7 (2016)
- Pages: 587-592
- Section: Article
- URL: https://journal-vniispk.ru/0038-0946/article/view/170651
- DOI: https://doi.org/10.1134/S003809461607008X
- ID: 170651
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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
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