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Методика орбитального построения спутниковой системы для решения задачи…

Инженерный журнал: наука и инновации

# 11·2017 13

A method of satellite constellations orbital construction

for operational global monitoring problem solution

© А.А. Lysenko, S.Yu. Ulybyshev

Central Scientific Research Institute of Chemistry and Mechanics,

Moscow, 115487, Russia

The article presents analytical calculations and numerical modeling results in the selec-

tion of optimal satellite constellations construction for operational global monitoring.

The article describes a method of satellite constellations construction orbital, the method

ensuring maximum break minimization in the observation of any point on the Earth's

surface for given survey characteristics from the spacecraft. We compared the results

obtained by different authors determining the maximum break minimization values in

observation for operational satellite constellations global monitoring for a given appa-

ratus number in the constellation and their survey characteristics. We showed that the

described methodology application for the satellite constellations construction, taking

into account onboard equipment specified characteristics, makes it possible to reduce the

problem to a one-parameter search for the best constellation system configuration from

the latitude argument of the satellites in it, and determine longitude of the ascending

node analytically. The obtained results make it possible to simplify the methodology for

searching the optimal satellite constellation configuration for a periodic global survey.

Keywords:

spacecraft, satellite constellation, operational global monitoring, one-route

satellite constellations, a break in the observation, inter-track offset, longitude of the as-

cending node

REFERENCES

[1]

Lang T.J. Walker Constellations to Minimize Revisit Time in Low Earth Orbit.

AAS/AIAA Space Flight Mechanics Meeting. Ponce, Puerto Rico, Feb. 9–13,

2003

. AAS 03-178. vol. 114, Univelt Inc., San Diego, 2003, pp. 1127–1143.

Advances in the Astronautical Sciences Series.

[2]

Razumny Y.N., Ermachenkov A.V.

Issledovanie Zemli iz kosmosa

Izvestiya,

Atmospheric and Oceanic Physics

, 1995, no. 2, pp. 57–70.

[3]

Saulskiy V.K.

Issledovanie Zemli iz kosmosa

Izvestiya,

Atmospheric and

Oceanic Physics

,

1989, no. 2, pp. 104–115.

[4]

Razoumny Y.N. New research methodology for Earth periodic coverage and

regularities in parametric localization of optimal low-Earth-orbit satellite

constellations.

Astrodynamics 2013

. S.B. Broschart, J.D. Turner, K.C. Howell,

F.R. Hoots, eds.

Proceedings of the AIAA/AAS Astrodynamics Specialist

Conference held August 11–15, 2013, Hilton Head, South Carolina, U.S.A

.

2014, vol. 150, pp. 3117–3136. Advances in the Astronautical Sciences Series.

[5]

Razoumny Y.N. Analytic solutions for Earth discontinuous coverage and

methods for analysis and synthesis of satellite orbits and constellations.

Proceedings of the AIAA/AAS Astrodynamics Specialist Conference, August 4–7,

2014, San-Diego, California, USA

. American Astronomical Society, 2014.

AIAA 2014–4160. DOI: 10.2514/6.2014-4160

[6]

Razoumny Y.N. Method of satellite orbit and constellation design for Earth

discontinuous coverage with minimal satellite Swath under the given constraint

on the maximum revisit time.

Advances in the Astronautical Sciences