Controlled solar sail transfers to near-Sun orbits with restrictions on sail temperature

Standard

Controlled solar sail transfers to near-Sun orbits with restrictions on sail temperature. / Koblik, V.; Polyakhova, E.; Sokolov, L.; Shmyrov, A.

в: Journal of the Astronautical Sciences, Том 47, № 3-4, 07.1999, стр. 189-206.

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

BibTeX

@article{b9641c801c9541b38b1c6802e8b57e42,

title = "Controlled solar sail transfers to near-Sun orbits with restrictions on sail temperature",

abstract = "We present results of numerical simulations of local-optimal trajectories of a space probe with a flat solar sail which moves from a circular Earth orbit to near-Sun regions. We examine the planar (ecliptic) and three-dimensional transfer cases. We consider the upper limit of the sail temperature as the basic restriction. The local-optimal control law of the sail orientation angle was chosen in such a way that the rate of decrease of the orbital focal parameter reaches its maximal value. In the three-dimensional case, the requirement of the maximization of the orbital plane rotation rate was added. We also investigated complex control modes of the sail orientation for near-Sun orbits and of some `falling onto the Sun' trajectories. These computer simulations allow us to examine the durations of some sail missions and to investigate the evolution of osculating elliptical orbits.",

author = "V. Koblik and E. Polyakhova and L. Sokolov and A. Shmyrov",

year = "1999",

month = jul,

language = "English",

volume = "47",

pages = "189--206",

journal = "Journal of the Astronautical Sciences",

issn = "0021-9142",

publisher = "Springer Nature",

number = "3-4",

}

RIS

TY - JOUR

T1 - Controlled solar sail transfers to near-Sun orbits with restrictions on sail temperature

AU - Koblik, V.

AU - Polyakhova, E.

AU - Sokolov, L.

AU - Shmyrov, A.

PY - 1999/7

Y1 - 1999/7

N2 - We present results of numerical simulations of local-optimal trajectories of a space probe with a flat solar sail which moves from a circular Earth orbit to near-Sun regions. We examine the planar (ecliptic) and three-dimensional transfer cases. We consider the upper limit of the sail temperature as the basic restriction. The local-optimal control law of the sail orientation angle was chosen in such a way that the rate of decrease of the orbital focal parameter reaches its maximal value. In the three-dimensional case, the requirement of the maximization of the orbital plane rotation rate was added. We also investigated complex control modes of the sail orientation for near-Sun orbits and of some `falling onto the Sun' trajectories. These computer simulations allow us to examine the durations of some sail missions and to investigate the evolution of osculating elliptical orbits.

AB - We present results of numerical simulations of local-optimal trajectories of a space probe with a flat solar sail which moves from a circular Earth orbit to near-Sun regions. We examine the planar (ecliptic) and three-dimensional transfer cases. We consider the upper limit of the sail temperature as the basic restriction. The local-optimal control law of the sail orientation angle was chosen in such a way that the rate of decrease of the orbital focal parameter reaches its maximal value. In the three-dimensional case, the requirement of the maximization of the orbital plane rotation rate was added. We also investigated complex control modes of the sail orientation for near-Sun orbits and of some `falling onto the Sun' trajectories. These computer simulations allow us to examine the durations of some sail missions and to investigate the evolution of osculating elliptical orbits.

UR - http://www.scopus.com/inward/record.url?scp=0033156460&partnerID=8YFLogxK

M3 - Article

AN - SCOPUS:0033156460

VL - 47

SP - 189

EP - 206

JO - Journal of the Astronautical Sciences

JF - Journal of the Astronautical Sciences

SN - 0021-9142

IS - 3-4

ER -

ID: 86488000