Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part I

V. V. Salmin; Салмин В. В.; V. V. Vasilyev; Васильев В. В.; S. A. Ishkov; Ишков С. А.; V. A. Romanenko; Романенко В. А.; V. O. Sokolov; Соколов В. О.; O. L. Starinova; Старинова О. Л.; V. V. Yurin; Юрин В. В.

doi:10.18287/2541-7533-2007-0-1(12)-37-52

Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part I

Authors: Salmin V.V.¹, Vasilyev V.V.¹, Ishkov S.A.¹, Romanenko V.A.¹, Sokolov V.O.¹, Starinova O.L.¹, Yurin V.V.¹
Affiliations:
1. Samara State Aerospace University
Issue: Vol 6, No 1 (2007)
Pages: 37-52
Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
URL: https://journals.ssau.ru/vestnik/article/view/477
DOI: https://doi.org/10.18287/2541-7533-2007-0-1(12)-37-52
ID: 477

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Abstract

The first part of the paper presents mathematical formulations of the tasks of optimizing flights of space vehicles with low-thrust engines and methods of their solution. The peculiarities of mathematical motionmodels used for control optimization within the frames of different tasks are discussed.