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Orbital maneuvers and space rendezvous. / Butikov, E.I.

In: Advances in Space Research, Vol. Volume 56, No. Issue 11, 2015, p. 2582-2594.

Research output: Contribution to journal › Article

Harvard

Butikov, EI 2015, 'Orbital maneuvers and space rendezvous', Advances in Space Research, vol. Volume 56, no. Issue 11, pp. 2582-2594. https://doi.org/10.1016/j.asr.2015.09.014

APA

Butikov, E. I. (2015). Orbital maneuvers and space rendezvous. Advances in Space Research, Volume 56(Issue 11), 2582-2594. https://doi.org/10.1016/j.asr.2015.09.014

Vancouver

Butikov EI. Orbital maneuvers and space rendezvous. Advances in Space Research. 2015;Volume 56(Issue 11):2582-2594. https://doi.org/10.1016/j.asr.2015.09.014

Author

Butikov, E.I. / Orbital maneuvers and space rendezvous. In: Advances in Space Research. 2015 ; Vol. Volume 56, No. Issue 11. pp. 2582-2594.

BibTeX

@article{45e8dad7e28a4a1584fcd6acc88f45fe,
title = "Orbital maneuvers and space rendezvous",
abstract = "Several possibilities of launching a space vehicle from the orbital station are considered and compared. Orbital maneuvers discussed in the paper can be useful in designing a trajectory for a specific space mission. The relative motion of orbiting bodies is investigated on examples of spacecraft rendezvous with the space station that stays in a circular orbit around the Earth. An elementary approach is illustrated by an accompanying simulation computer program and supported by a mathematical treatment based on fundamental laws of physics and conservation laws. Material is appropriate for engineers and other personnel involved in space exploration, undergraduate and graduate students studying classical physics and orbital mechanics.",
keywords = "Keplerian orbits, Space navigation, Impulsive maneuvers, Hohmann{\textquoteright}s transitions, Soft docking",
author = "E.I. Butikov",
year = "2015",
doi = "10.1016/j.asr.2015.09.014",
language = "English",
volume = "Volume 56",
pages = "2582--2594",
journal = "Advances in Space Research",
issn = "0273-1177",
publisher = "Elsevier",
number = "Issue 11",

}

RIS

TY - JOUR

T1 - Orbital maneuvers and space rendezvous

AU - Butikov, E.I.

PY - 2015

Y1 - 2015

N2 - Several possibilities of launching a space vehicle from the orbital station are considered and compared. Orbital maneuvers discussed in the paper can be useful in designing a trajectory for a specific space mission. The relative motion of orbiting bodies is investigated on examples of spacecraft rendezvous with the space station that stays in a circular orbit around the Earth. An elementary approach is illustrated by an accompanying simulation computer program and supported by a mathematical treatment based on fundamental laws of physics and conservation laws. Material is appropriate for engineers and other personnel involved in space exploration, undergraduate and graduate students studying classical physics and orbital mechanics.

AB - Several possibilities of launching a space vehicle from the orbital station are considered and compared. Orbital maneuvers discussed in the paper can be useful in designing a trajectory for a specific space mission. The relative motion of orbiting bodies is investigated on examples of spacecraft rendezvous with the space station that stays in a circular orbit around the Earth. An elementary approach is illustrated by an accompanying simulation computer program and supported by a mathematical treatment based on fundamental laws of physics and conservation laws. Material is appropriate for engineers and other personnel involved in space exploration, undergraduate and graduate students studying classical physics and orbital mechanics.

KW - Keplerian orbits

KW - Space navigation

KW - Impulsive maneuvers

KW - Hohmann’s transitions

KW - Soft docking

U2 - 10.1016/j.asr.2015.09.014

DO - 10.1016/j.asr.2015.09.014

M3 - Article

VL - Volume 56

SP - 2582

EP - 2594

JO - Advances in Space Research

JF - Advances in Space Research

SN - 0273-1177

IS - Issue 11

ER -

ID: 3978214