Standard

Maneuvering in Near-Earth Space with the Use of the Collinear Libration Points. / Shmyrov, Alexander; Shymanchuk, Dzmitry.

2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOVS READING. ed. / AA Tikhonov. Institute of Electrical and Electronics Engineers Inc., 2015.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review

Harvard

Shmyrov, A & Shymanchuk, D 2015, Maneuvering in Near-Earth Space with the Use of the Collinear Libration Points. in AA Tikhonov (ed.), 2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOVS READING. Institute of Electrical and Electronics Engineers Inc., 2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOV'S READING, Saint Petersburg, Russian Federation, 2/02/15.

APA

Shmyrov, A., & Shymanchuk, D. (2015). Maneuvering in Near-Earth Space with the Use of the Collinear Libration Points. In AA. Tikhonov (Ed.), 2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOVS READING Institute of Electrical and Electronics Engineers Inc..

Vancouver

Shmyrov A, Shymanchuk D. Maneuvering in Near-Earth Space with the Use of the Collinear Libration Points. In Tikhonov AA, editor, 2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOVS READING. Institute of Electrical and Electronics Engineers Inc. 2015

Author

Shmyrov, Alexander ; Shymanchuk, Dzmitry. / Maneuvering in Near-Earth Space with the Use of the Collinear Libration Points. 2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOVS READING. editor / AA Tikhonov. Institute of Electrical and Electronics Engineers Inc., 2015.

BibTeX

@inproceedings{f4d8c11891934fd3883dadb6010f8058,
title = "Maneuvering in Near-Earth Space with the Use of the Collinear Libration Points",
abstract = "The use of the neighborhood of collinear libration point (L-1 or L-2()) of the Sun-Earth system has long been of practical importance in connection with projects implemented by NASA and ESA. A celestial body motion is considered in a rotating frame within the Hill's problem of the circular restricted three-body problem. It is known that collinear libration points are unstable but its instability can be used as a positive factor for maneuvering a celestial body in the near-Earth space. For example, it may be used to solve the problem of comet and asteroid hazard to monitor space objects posing threat to the Earth. We offer a methodology for constructing control algorithms for the orbital motion of a celestial body. This methodology is based on the properties of a specially introduced phase variables function called {"}hazard function{"}. Numerical simulation results are given.",
author = "Alexander Shmyrov and Dzmitry Shymanchuk",
year = "2015",
language = "Английский",
editor = "AA Tikhonov",
booktitle = "2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOVS READING",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
address = "Соединенные Штаты Америки",
note = "null ; Conference date: 02-02-2015 Through 06-02-2015",
url = "http://pol2015.math.spbu.ru/en/, http://pol2015.math.spbu.ru/en/about/, http://pol2015.math.spbu.ru/",

}

RIS

TY - GEN

T1 - Maneuvering in Near-Earth Space with the Use of the Collinear Libration Points

AU - Shmyrov, Alexander

AU - Shymanchuk, Dzmitry

N1 - Conference code: 7

PY - 2015

Y1 - 2015

N2 - The use of the neighborhood of collinear libration point (L-1 or L-2()) of the Sun-Earth system has long been of practical importance in connection with projects implemented by NASA and ESA. A celestial body motion is considered in a rotating frame within the Hill's problem of the circular restricted three-body problem. It is known that collinear libration points are unstable but its instability can be used as a positive factor for maneuvering a celestial body in the near-Earth space. For example, it may be used to solve the problem of comet and asteroid hazard to monitor space objects posing threat to the Earth. We offer a methodology for constructing control algorithms for the orbital motion of a celestial body. This methodology is based on the properties of a specially introduced phase variables function called "hazard function". Numerical simulation results are given.

AB - The use of the neighborhood of collinear libration point (L-1 or L-2()) of the Sun-Earth system has long been of practical importance in connection with projects implemented by NASA and ESA. A celestial body motion is considered in a rotating frame within the Hill's problem of the circular restricted three-body problem. It is known that collinear libration points are unstable but its instability can be used as a positive factor for maneuvering a celestial body in the near-Earth space. For example, it may be used to solve the problem of comet and asteroid hazard to monitor space objects posing threat to the Earth. We offer a methodology for constructing control algorithms for the orbital motion of a celestial body. This methodology is based on the properties of a specially introduced phase variables function called "hazard function". Numerical simulation results are given.

M3 - статья в сборнике материалов конференции

BT - 2015 INTERNATIONAL CONFERENCE ON MECHANICS SEVENTH POLYAKHOVS READING

A2 - Tikhonov, AA

PB - Institute of Electrical and Electronics Engineers Inc.

Y2 - 2 February 2015 through 6 February 2015

ER -

ID: 9426736