Determination of the optimal mode of operation of the small thrust motors of a maneuvering spacecraft

V. I. Bimatov, I. A. Druzhinin, I. V. Druzhinina, E. E. Libin, S. V. Chakhlov

Center for Industrial Tomography

Research output: Contribution to journal › Article › peer-review

Abstract

We consider the problem of constructing an optimal cyclogram for the small-thrust rocket motors that govern the descent of a spacecraft to earth or other orbital maneuvers. The problem is solved by the perturbation method, the perturbation in this case being the ratio of the thrust of the motor to the weight of the spacecraft.

Original language	English
Pages (from-to)	237-243
Number of pages	7
Journal	Computational Mathematics and Modeling
Volume	9
Issue number	3
DOIs	https://doi.org/10.1007/BF02407143
Publication status	Published - 1998

ASJC Scopus subject areas

Computational Mathematics

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10.1007/BF02407143

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title = "Determination of the optimal mode of operation of the small thrust motors of a maneuvering spacecraft",

abstract = "We consider the problem of constructing an optimal cyclogram for the small-thrust rocket motors that govern the descent of a spacecraft to earth or other orbital maneuvers. The problem is solved by the perturbation method, the perturbation in this case being the ratio of the thrust of the motor to the weight of the spacecraft.",

author = "Bimatov, {V. I.} and Druzhinin, {I. A.} and Druzhinina, {I. V.} and Libin, {E. E.} and Chakhlov, {S. V.}",

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AU - Bimatov, V. I.

AU - Druzhinin, I. A.

AU - Druzhinina, I. V.

AU - Libin, E. E.

AU - Chakhlov, S. V.

PY - 1998

Y1 - 1998

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AB - We consider the problem of constructing an optimal cyclogram for the small-thrust rocket motors that govern the descent of a spacecraft to earth or other orbital maneuvers. The problem is solved by the perturbation method, the perturbation in this case being the ratio of the thrust of the motor to the weight of the spacecraft.

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Determination of the optimal mode of operation of the small thrust motors of a maneuvering spacecraft

Abstract

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