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Design of Satellite Constellations for Operational Global Monitoring with a Daily Repeat of Flight Track

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Abstract

An analytical technique for designing satellite constellations for operational global monitoring of Earth’s surface is presented. This technique makes it possible to calculate the rational shift from the argument of latitude and longitude of the right ascension of the ascending node between satellites in the system. The orbital parameters of spacecraft and the characteristics of its field of view should be taken from basic solutions for satellite constellations of operational global monitoring, considered by authors in earlier studies. The resulting basic solutions make it possible to find the maximal break in the observation of any point on Earth’s surface for a single satellite, and the technique described here makes it possible to determine the rational location of several satellites in the system and minimize the peak revisit time for the entire satellite constellation. The technique has been developed for spacecraft with a daily repeat of flight track and makes it possible to determine the minimum number of satellites in the system that can provide a break in observation to be limited by a given value. This study presents several families of solutions for satellite constellations with a daily repeat of flight track on low circular orbits at heights below 2000 km.

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REFERENCES

  1. Lang, T.J., LEO constellations to cover the Earth in one rev, in AIAA/AAS Astrodynamics Specialist Conference, 4–7 August 2014, San Diego, 2014, AIAA-4156.

  2. Mozhaev, G.V., Sintez orbital’nykh struktur sputnikovykh sistem (Synthesis of Orbital Structures of Satellite Constellations), Moscow: Mashinostroenie, 1989.

  3. Lang, T.J., Walker constellations to minimize revisit time in low earth orbit, in Proceedings of the AAS/AIAA Astrodynamics Conference, 2003, AAS03-178.

  4. Byrkov, B.P. and Razumnyi, Yu.N., Analytic technique for determining the Earth’s surveying periodicity by a satellite of the system for the study of exploration of the Earth’s natural resources, Issled. Zemli Kosmosa, 1992, no. 2, pp. 91–97.

  5. Razumnyi, Yu.N. and Ermachenkov, A.V., Analytic technique for determining the discontinuous coverage of the Earth by a satellite constellation and rational orbital constructs for solving problems in the study of the Earth’s natural resources, Issled. Zemli Kosmosa, 1995, no. 2, pp. 57–70.

  6. Razumnyi, Yu.N., A method of the optimization of parameters of single-path satellite constellations for periodic surveying of the Earth, Issled. Zemli Kosmosa, 1991, no. 5, pp. 39–46.

  7. Saul’skii, V.K., Optimal orbits and the structure of satellite constellations for periodic surveying of the Earth, Issled. Zemli Kosmosa, 1989, no. 2, pp. 104–115.

  8. Saul’skii, V.K. and Lukashevich, E.L., Choice of satellite orbits for full-time global surveying of the Earth, Issled. Zemli Kosmosa, 1984, no. 1, pp. 110–118.

  9. Razoumny, Y.N., New research methodology for earth periodic coverage and regularities in parametric localization of optimal low-Earth-orbit satellite constellations, Adv. Astronaut. Sci. Ser., 2014, vol. 125, pp. 3117–3136.

    Google Scholar 

  10. Razoumny, Y.N., Method for satellite orbit and constellation design for Earth discontinuous coverage with minimal satellite Swath under the given constraint on the maximum revisit time, Adv. Astronaut. Sci. Ser., 2015, vol. 129, pp. 2337–2356.

    Google Scholar 

  11. Razoumny, Y.N., Fundamentals of the route theory for satellite constellation design for Earth discontinuous coverage. Part 1: Analytic emulation of the Earth coverage, Acta Astronaut., 2016, vol. 128, pp. 722–740.

    Article  ADS  Google Scholar 

  12. George, E., Optimization of satellite constellations for discontinuous global coverage via genetic algorithms, Adv. Astronaut. Sci. Ser., AAS/AIAA Astrodynamics Specialist Conference 1997, San Diego: Univelt Inc., 1998, vol. 97, AAS97-621.

  13. Williams, E.A., Crossley, W.A., and Lang, T.J., Average and maximum revisit time trade studies for satellite constellations using a multiobjective genetic algorithm, Adv. Astronaut. Sci. Ser., AAS/AIAA Space Flight Mechanics Meeting, Clearwater, Florida, January 23–26, 2000, San Diego: Univelt Inc., 2000, vol. 105, AAS00-139, pp. 653–667.

  14. Lang, T.J., An “adjacent swatch” method to design efficient LEO constellations, AAS Astrodynamics Specialist Conference, 4–6 February 2016, San Diego, California, 2016, AAS16-203.

  15. Ulybyshev, Y., Satellite constellation design for complex coverage, AIAA J. Spacecraft Rockets, 2008, vol. 45, no. 4, pp. 843–849.

    Article  ADS  Google Scholar 

  16. Ulybyshev, Y., Geometric analysis and design method for discontinuous coverage satellite constellations, J. Guid. Control Dyn., 2014, vol. 37, no. 4, pp. 549–557.

    Article  ADS  Google Scholar 

  17. Ulybyshev, Y., General analysis method for discontinuous coverage satellite constellations, J. Guid. Control Dyn., 2015, vol. 38, no. 12, pp. 2475–2482.

    Article  ADS  Google Scholar 

  18. Saul’skii, V.K., A vector method for synthesis of orbits and the structure of satellite constellations for multiswath periodic coverage of the Earth, Cosmic Res., 2016, vol. 54, no. 4, pp. 313–324.

    Article  ADS  Google Scholar 

  19. Gorbunov, A.V. and Saul’skii, V.K., The use of the vector model of the Earth’s coverage for satellite analysis on iso-path orbits, Vopr. Elektromekh. Tr. VNIIEM, 2017, vol. 153, no. 4, pp. 29–46.

    Google Scholar 

  20. Saul’skii, V.K., Analysis of satellite systems for the periodic survey of the Earth, Cosmic Res., 2017, vol. 55, no. 4, pp. 275–289.

    Article  ADS  Google Scholar 

  21. Lysenko, A.A. and Ulybyshev, S.Yu., Choice of spacecraft orbit parameters for operational global monitoring of the Earth’s surface, Kosmonavt. Raketostr., 2016, no. 5, pp. 45–56.

  22. Ulybyshev, S.Yu., The use of Sun-synchronous orbits for a real-time global coverage satellite, Cosmic Res., 2016, vol. 54, no. 6, pp. 445–451.

    Article  ADS  Google Scholar 

  23. Lysenko, A.A. and Ulybyshev, S.Yu., A technique of orbital construction of satellite systems for operational global monitoring, Inzh. Zh.: Nauka Innovatsii, no. 11. https://doi.org/10.18698/2308-6033-2017-11-1699

  24. Satellite Tool Kit: Users Guide, Malvern, USA: Analytical Graphics Inc., 2000.

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Authors and Affiliations

  1. Central Scientific Research Institute of Chemistry and Mechanics,, 115487, Moscow, Russia

    S. Yu. Ulybyshev & A. A. Lysenko

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  1. S. Yu. Ulybyshev
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  2. A. A. Lysenko
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Correspondence to S. Yu. Ulybyshev.

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Translated by V. Arutyunyan

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Ulybyshev, S.Y., Lysenko, A.A. Design of Satellite Constellations for Operational Global Monitoring with a Daily Repeat of Flight Track. Cosmic Res 57, 204–212 (2019). https://doi.org/10.1134/S0010952519030080

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  • DOI: https://doi.org/10.1134/S0010952519030080

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