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

Access to Document

10.1007/BF02407143

Fingerprint Dive into the research topics of 'Determination of the optimal mode of operation of the small thrust motors of a maneuvering spacecraft'. Together they form a unique fingerprint.

Cite this

@article{f30923cc90064bd797e9591ae2468434,

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.}",

year = "1998",

doi = "10.1007/BF02407143",

language = "English",

volume = "9",

pages = "237--243",

journal = "Computational Mathematics and Modeling",

issn = "1046-283X",

publisher = "Springer New York",

number = "3",

}

TY - JOUR

T1 - Determination of the optimal mode of operation of the small thrust motors of a maneuvering spacecraft

AU - Bimatov, V. I.

AU - Druzhinin, I. A.

AU - Druzhinina, I. V.

AU - Libin, E. E.

AU - Chakhlov, S. V.

PY - 1998

Y1 - 1998

N2 - 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.

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.

UR - http://www.scopus.com/inward/record.url?scp=54749143235&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=54749143235&partnerID=8YFLogxK

U2 - 10.1007/BF02407143

DO - 10.1007/BF02407143

M3 - Article

AN - SCOPUS:54749143235

VL - 9

SP - 237

EP - 243

JO - Computational Mathematics and Modeling

JF - Computational Mathematics and Modeling

SN - 1046-283X

IS - 3

ER -