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PROSPECTS OF PHOTOGRAVITATIONAL CELESTIAL MECHANICS FOR SPACE SYSTEMS
Abstract
The possibilities and prospects of a solar sail using to solve new problems of space systems control are discussed. The economic and environmental benefits that can be obtained with this control method for interplanetary transitions or for the functioning of the space system in the near-planetary space are considered. This type of control is carried out through the use of special solar sail designs that allow the maximum use of light pressure. The very idea of the solar sail control is connected with the search for new ways to use solar energy, as well as with the expansion of the nanotechnology application field on Earth and in space. When designing the solar sail, the possibility is immediately taken into account that when it is deployed to its working position in orbit, it will be used to control the spacecraft (SC) during flight. At the same time, the question of the physical and optical properties of the real sail in space conditions is extremely important. The use of new technologies to significantly improve such properties should contribute to the prospect of the solar sail possible use as a space engine based on the direct use of an unlimited solar radiation energy source.
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References7
Polyakhova E.N. Space flight with a solar sail. Ed. V.A. Egorov. M.: Science. 1986, 304 pp. 2nd ed., M. Ed. house "Librocom" (URSS). 2011. 320 p., 3rd ed. ster.: Book House. "Librokom". 2018. 320 p.
Shmyrov A.S., Polyakhova E.N., Mathematical substantiation of the theory of orbital correction performed with the help of a solar sail // Space Research. 1989. No. 1. T. 27. Pp. 54-63.
Korolev V.S., Polyakhova E.N., The Solar Sail: Current State of the Problem. // Intern. Conf. on Mechanics "Eights Polyakhov Readings", St.Petersburg, Russia. AIP Conf. Proceedings: 1959, 040014 (2018); DOI 10.1063 / 1.5034617.
Pototskaya I., Polyakhova, E., Korolev, V., Problems of control motion and stability of solar sail spacecraft, 2017, International Multidisciplinary Scientific GeoConference Surveying Geology and Mining Ecology Management, SGEM. 17, 62, pp. 939-946. DOI: 10.5593/sgem2017/62/s28.120
Tsander F.A., Problems of Spaceflights with Jet Propulsion Engines: Interplanetary Travels, (in Russia), 1961,.459 p.
Shymanchuk D.V., On the Coupled Orbit-Attitude Control Motion of a Celestial Body in the Neighborhood of the Collinear Libration Point L1 of the Sun-Earth System, Constructive Nonsmooth Analysis and Related Topics, (International Conference, Dedicated to the Memory of V.F. Demyanov), Proceedings, IEEE Inc., p.7974013, 2017. DOI: 10.1109/cnsa.2017.7974013
Egorov V.A., Pomazanov M.V., Solar Sail: the Principles of Design, Control and flights to asteroids. (in Russia), 1997, 87 p.
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