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The interception problem of a celestial body with the use of the collinear libration points. / Shmyrov, A.; Shymanchuk, D.; Sokolov, L.

2015 International Conference on "Stability and Control Processes" in Memory of V.I. Zubov, SCP 2015 - Proceedings. 2015. стр. 129-131.

Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная

Harvard

Shmyrov, A, Shymanchuk, D & Sokolov, L 2015, The interception problem of a celestial body with the use of the collinear libration points. в 2015 International Conference on "Stability and Control Processes" in Memory of V.I. Zubov, SCP 2015 - Proceedings. стр. 129-131, III Международная конференция "Устойчивость и процессы управления", посвященная 85-летию со дня рождения чл.-корр. РАН В.И. Зубова, St. Petersburg, Российская Федерация, 5/10/15. https://doi.org/10.1109/SCP.2015.7342068

APA

Shmyrov, A., Shymanchuk, D., & Sokolov, L. (2015). The interception problem of a celestial body with the use of the collinear libration points. в 2015 International Conference on "Stability and Control Processes" in Memory of V.I. Zubov, SCP 2015 - Proceedings (стр. 129-131) https://doi.org/10.1109/SCP.2015.7342068

Vancouver

Shmyrov A, Shymanchuk D, Sokolov L. The interception problem of a celestial body with the use of the collinear libration points. в 2015 International Conference on "Stability and Control Processes" in Memory of V.I. Zubov, SCP 2015 - Proceedings. 2015. стр. 129-131 https://doi.org/10.1109/SCP.2015.7342068

Author

Shmyrov, A. ; Shymanchuk, D. ; Sokolov, L. / The interception problem of a celestial body with the use of the collinear libration points. 2015 International Conference on "Stability and Control Processes" in Memory of V.I. Zubov, SCP 2015 - Proceedings. 2015. стр. 129-131

BibTeX

@inproceedings{091c999036664e7b8fc24d672201235a,
title = "The interception problem of a celestial body with the use of the collinear libration points",
abstract = "{\textcopyright} 2015 IEEE.This paper studies the problem of an intercept trajectory construction when using the neighborhood of the collinear libration point L1 of the Sun-Earth system. 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. Development methodology of control algorithms for the orbital motion of a celestial body when using the instability of collinear libration points is offered. The construction of an intercept trajectory is based on the properties of a specially introduced phase variables function, called 'hazard function'. The results of the numerical integration are graphically illustrated.",
author = "A. Shmyrov and D. Shymanchuk and L. Sokolov",
year = "2015",
doi = "10.1109/SCP.2015.7342068",
language = "English",
isbn = "9781467376983",
pages = "129--131",
booktitle = "2015 International Conference on {"}Stability and Control Processes{"} in Memory of V.I. Zubov, SCP 2015 - Proceedings",
note = "International Conference on {"}Stability and Control Processes{"} in Memory of V.I. Zubov, SCP 2015 ; Conference date: 05-10-2015 Through 09-10-2015",
url = "http://www.apmath.spbu.ru/scp2015/openconf.php",

}

RIS

TY - GEN

T1 - The interception problem of a celestial body with the use of the collinear libration points

AU - Shmyrov, A.

AU - Shymanchuk, D.

AU - Sokolov, L.

PY - 2015

Y1 - 2015

N2 - © 2015 IEEE.This paper studies the problem of an intercept trajectory construction when using the neighborhood of the collinear libration point L1 of the Sun-Earth system. 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. Development methodology of control algorithms for the orbital motion of a celestial body when using the instability of collinear libration points is offered. The construction of an intercept trajectory is based on the properties of a specially introduced phase variables function, called 'hazard function'. The results of the numerical integration are graphically illustrated.

AB - © 2015 IEEE.This paper studies the problem of an intercept trajectory construction when using the neighborhood of the collinear libration point L1 of the Sun-Earth system. 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. Development methodology of control algorithms for the orbital motion of a celestial body when using the instability of collinear libration points is offered. The construction of an intercept trajectory is based on the properties of a specially introduced phase variables function, called 'hazard function'. The results of the numerical integration are graphically illustrated.

U2 - 10.1109/SCP.2015.7342068

DO - 10.1109/SCP.2015.7342068

M3 - Conference contribution

SN - 9781467376983

SP - 129

EP - 131

BT - 2015 International Conference on "Stability and Control Processes" in Memory of V.I. Zubov, SCP 2015 - Proceedings

T2 - International Conference on "Stability and Control Processes" in Memory of V.I. Zubov, SCP 2015

Y2 - 5 October 2015 through 9 October 2015

ER -

ID: 4013497