Controlled solar sailing transfer flights into near-Sun orbits under restrictions on sail temperature

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Controlled solar sailing transfer flights into near-Sun orbits under restrictions on sail temperature. / Koblik, V. V.; Polyakhova, E. N.; Sokolov, L. L.; Shmyrov, A. S.

в: Cosmic Research, Том 34, № 6, 11.1996, стр. 572-578.

Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование

BibTeX

@article{a88de3fe00ae442f8defaac50150eebc,

title = "Controlled solar sailing transfer flights into near-Sun orbits under restrictions on sail temperature",

abstract = "We discuss numerical construction results of locally optimal spacecraft trajectories with a plane solar sail from Earth's circular orbit into near-Sun space. Both the planar (ecliptic) and three-dimensional cases of sailing are examined. The maximum allowable temperature is taken to be the main restriction. The locally optimal control of sail attitude is chosen for the highest decrease rate of the focal parameter for the spacecraft's osculating orbit. In the three-dimensional case, the requirement for the highest rate of orbital plane rotation is included. Complex schemes of sail attitude control are elaborated to attain various types of near-Sun orbits, as well as trajectories for {"}falling{"} onto the Sun. Numerical investigations permit flight time determination to required orbits and to study the evolution of osculating orbits.",

author = "Koblik, {V. V.} and Polyakhova, {E. N.} and Sokolov, {L. L.} and Shmyrov, {A. S.}",

year = "1996",

month = nov,

language = "English",

volume = "34",

pages = "572--578",

journal = "Cosmic Research",

issn = "0010-9525",

publisher = "МАИК {"}Наука/Интерпериодика{"}",

number = "6",

}

RIS

TY - JOUR

T1 - Controlled solar sailing transfer flights into near-Sun orbits under restrictions on sail temperature

AU - Koblik, V. V.

AU - Polyakhova, E. N.

AU - Sokolov, L. L.

AU - Shmyrov, A. S.

PY - 1996/11

Y1 - 1996/11

N2 - We discuss numerical construction results of locally optimal spacecraft trajectories with a plane solar sail from Earth's circular orbit into near-Sun space. Both the planar (ecliptic) and three-dimensional cases of sailing are examined. The maximum allowable temperature is taken to be the main restriction. The locally optimal control of sail attitude is chosen for the highest decrease rate of the focal parameter for the spacecraft's osculating orbit. In the three-dimensional case, the requirement for the highest rate of orbital plane rotation is included. Complex schemes of sail attitude control are elaborated to attain various types of near-Sun orbits, as well as trajectories for "falling" onto the Sun. Numerical investigations permit flight time determination to required orbits and to study the evolution of osculating orbits.

AB - We discuss numerical construction results of locally optimal spacecraft trajectories with a plane solar sail from Earth's circular orbit into near-Sun space. Both the planar (ecliptic) and three-dimensional cases of sailing are examined. The maximum allowable temperature is taken to be the main restriction. The locally optimal control of sail attitude is chosen for the highest decrease rate of the focal parameter for the spacecraft's osculating orbit. In the three-dimensional case, the requirement for the highest rate of orbital plane rotation is included. Complex schemes of sail attitude control are elaborated to attain various types of near-Sun orbits, as well as trajectories for "falling" onto the Sun. Numerical investigations permit flight time determination to required orbits and to study the evolution of osculating orbits.

UR - http://www.scopus.com/inward/record.url?scp=0343237493&partnerID=8YFLogxK

M3 - Article

AN - SCOPUS:0343237493

VL - 34

SP - 572

EP - 578

JO - Cosmic Research

JF - Cosmic Research

SN - 0010-9525

IS - 6

ER -

ID: 86488157