Article

Cover

Title

Conception of moon satellite navigation system building

Authors

V.E. Chebotarev, V.I. Kudimov, A.V. Konyaev

Organization

JSC Academician M. F. Reshetnev Information Satellite Systems
Zheleznogorsk, Krasnoyarsk region, Russian Federation

Abstract

The analysis of the problems of Selenodezic support of lunar satellite navigation systems is carried out. The implemented methods of ballistic support of near-Earth navigation satellites in terms of the possibility of their application for lunar satellite navigation systems are considered. When constructing a selenocentric coordinate system, it is proposed to use methods of creating a matching model of the gravitational field developed for terrestrial navigation systems and increasing the accuracy of the analytic theory of motion. The method of information compression was proposed to improve the speed of transmission of the results of the measurement of current navigation parameters obtained over the entire visible portion of the orbit. High-precision analytical theory of motion was developed to increase the speed of the solution of the problem of clarifying the initial conditions of motion. The automated complex for determining orbits on the basis of analytical methods was created to perform the formulated work to ensure proper accuracy. To start work on the construction of a selenocentric coordinate system, it is enough to launch 1-2 satellites to the near-moon orbit and deploy a network of 3-4 selenodezic points. Software in the Global Navigation Satellite Systems can be organized on a personal computer.

Keywords

Moon, moon satellite navigation system, moon station, navigation

References

[1] Shebshaevich V. S. Dmitriev P. P., Ivantsevich N. V. Setevye sputnikovye radionavigacionnye sistemy [Networked satellite radio navigation systems]. Moscow, Radio and Communication, 1993. 408 p. (In Russian)

[2] Varaksina N. Yu. Creation of the navigation support network on the lunar surface in the fundamental coordinate system : Cand. Diss. Kazan, 2013, 205 p.

[3] Venikov V. A. Teoriya podobiya i modelirovaniya [Theory of similarity and modeling]. Moscow, Higher School, 1976. 479 p. (In Russian)

[4] Sagitov M. U. Lunnaya gravimetriya [Moonlight gravimetry]. Moscow, The main editorial board of the physical and mathematical literature of the Nauka Publishers, 1979. 432 p. (In Russian)

[5] Volosov P. S., Volynkin L. I., Mishchenko I. N. Sputnikovaya radionavigacionnaya sistema «Tranzit» [Satellite radio navigation system «Transit»] // Foreign radioelectronics, 1980, no. 8. (In Russian)

[6] Kudymov V.I. Vyvod soglasuyushchej modeli geopotenciala dlya orbit geodezicheskih apparatov [Derivation of the matching geopotential model for the orbits of geodetic devices] // Geodesy and Cartography, 1990, no. 4, pp. 14–16. (In Russian)

[7] Akim E. L. Pole tyagoteniya Luny i dvizhenie ee iskusstvennyh sputnikov [The gravitational field of the Moon and the motion of its artificial satellites]. Мoscow, Mechanical Engineering, 1984. 288 p. (In Russian)

[8] Grushinsky N.P. Gravitacionnaya razvedka [Gravitational exploration]. Moscow, Nedra, 1988. 369 p. (In Russian)

[9] Demin V.G. Dvizhenie iskusstvennogo sputnika v necentral'nom pole tyagoteniya [Motion of an artificial satellite in an off-center gravitational field]. Izhevsk, RDE Regular and chaotic dynamics, 2010. 420 p. (In Russian)

[10] Pellinen L. P. Vysshaya geodeziya [Higher Geodesy]. Moscow, Nedra, 1978. 264 p. (In Russian)

[11] Chebotarev V.E., Zvonar D.V., Gritsan O.B., Vnukov A.A. Concept of triangulation selenodesy network design // The Research of the Science City, 2014, no. 2, pp. 4–9. (In Russian)

[12] Chebotarev V.E., Kudymov V.I., Zvonar V.D., Vnukov A.A., Vladimirov A.V. Circumlunar navigation // The Research of the Science City, 2014, no. 4, pp. 14–20. (In Russian)

For citing this article

Chebotarev V.E., Kudimov V.I., Konyaev A.V. Conception of moon satellite navigation system building // Spacecrafts & Technologies, 2018, vol. 2, no. 2, pp. 79-83. doi: 10.26732/2618-7957-2018-2-79-83

This Article is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License (CC BY-NC 4.0).