Journal of Astronomy and Space Sciences

  • 제39권3호
  • /
  • Pages.109-116
  • /
  • 2022
  • /
  • 2093-5587(pISSN)
  • /
  • 2093-1409(eISSN)
한국우주과학회 (The Korean Space Science Society)
권호 표지
DOI QR코드

DOI QR Code

Feasibility Study of Communication Access via Iridium Constellation for Small-Scale Magnetospheric Ionospheric Plasma Experiment Mission

  • Song, Hosub (Korea Astronomy and Space Science Institute) ;
  • Lee, Jaejin (Korea Astronomy and Space Science Institute) ;
  • Yi, Yu (Department of Astronomy, Space Science and Geology, Chungnam National University)
  • 투고 : 2022.07.13
  • 심사 : 2022.08.31
  • 발행 : 2022.09.15
PDF 다운로드
⟨ 이전 논문 다음 논문 ⟩

초록

The small-scale magnetospheric and ionospheric plasma experiment (SNIPE) is a mission initiated by the Korea Astronomy and Space Science Institute (KASI) in 2017 and comprises four 6U-sized nano-satellites (Korea Astronomy and Space Science Institute Satellite-1, KASISat-1) flying in formations. The main goal of the SNIPE mission is to investigate the space environment in low Earth orbit at 500-km. Because Iridium & GPS Board (IGB) is installed on the KASISat-1, a communication simulation is required to analyze the contact number and the duration. In this study, communication simulations between the Iridium satellite network and KASISat-1 are performed using STK Pro (System Tool Kit Pro Ver 11.2) from the AGI (Analytical Graphics, Inc.). The contact number and durations were analyzed by each orbit and date. The analysis shows that the average access number per day is 38.714 times, with an average of 2.533 times per orbit for a week. Furthermore, on average, the Iridium satellite communication is linked for 70.597 min daily. Moreover, 4.625 min is the average duration of an individual orbit.

키워드

과제정보

This research was supported by the Korea Astronomy and Space Science Institute under the R&D program (Project No. 2022-1-850-08) supervised by the Ministry of Science and ICT. This research is based on the master's thesis of the first author (2019, "Communication accessibility between SNIPE nano-satellite and iridium satellite constellation").

참고문헌

  1. Allmen J, Petro A, Small spacecraft technology, Proceedings of the AIAA/USU Conference on Small Satellites, Logan, UT, 4-7 Aug 2014.
  2. Brunt P, IRIDIUM®: overview and status, Space Commun. 14, 61-68 (1996).
  3. Cho DH, Kim H, Kim HD, Visibility analysis of iridium communication for SNIPE nano-satellite, J. Korean Soc. Aeronaut. Space Sci. 50, 127-135 (2022). https://doi.org/10.5139/JKSAS.2022.50.2.127
  4. Claybrook JR, Feasibility analysis on the utilization of the Iridium Satellite Communications Network for resident space objects in Low Earth Orbit, Master Thesis, Air Force Institute of Technology (2013).
  5. Corpino S, Tomasicchio G, Di Donna AM, Satellite communication channel model for rotary-wing vehicles in a mission analysis context (2022) [Internet], viewed 2022 Jul 20, available from: https://webthesis.biblio.polito.it/22340/1/tesi.pdf
  6. Dahal UD, Cost-effective microcontroller-based iridium satellite communication architecture for a remote renewable energy source, Master Thesis, Bharathiar University (2002).
  7. Fossa CE, Raines RA, Gunsch GH, Temple MA, An overview of the IRIDIUM (R) low Earth orbit (LEO) satellite system, Proceedings of the IEEE 1998 National Aerospace and Electronics Conference, Dayton, OH, 17 Jul 1998.
  8. Kang S, Song Y, Park SY, Nanosat formation flying design for SNIPE mission, J. Astron. Space Sci. 37, 51-60 (2020). https://doi.org/10.5140/JASS.2020.37.1.51
  9. Khan K, Data communication with a nano-satellite using satellite personal communication networks (s-pcns), Master Thesis, University of Central Florida (2008).
  10. Kim HD, Choi WS, Kim MK, Kim JH, Kim KD, et al., Design and development of the SNIPE bus system, J. Space Technol. Appl. 2, 81-103 (2022). https://doi.org/10.52912/jsta.2022.2.2.81
  11. Kim JS, Kim HD, Development of drag augmentation device for post mission disposal of nanosatellite, J. Space Technol. Appl. 2, 1-12 (2022). https://doi.org/10.52912/jsta.2022.2.1.1
  12. Lee J, Sohn J, Park J, Yang TY, Song HS, et al., SNIPE mission for space weather research, J. Space Technol. Appl. 2, 104-120 (2022). https://doi.org/10.52912/jsta.2022.2.2.104
  13. Maine K, Devieux C, Swan P, Overview of IRIDIUM satellite network, Proceedings of the WESCON'95, San Francisco, CA, 7-9 Nov 1995.
  14. Pratt SR, Raines RA, Fossa CE, Temple MA, An operational and performance overview of the IRIDIUM low earth orbit satellite system, IEEE Commun. Surv. 2, 2-10 (1999). http://doi.org/10.1109/COMST.1999.5340513
  15. Riot VJ, Simms LM, Carter D, Lessons learned using iridium to communicate with a CubeSat in low earth orbit, J. Small Satell. 10, 995-1006 (2021).
  16. Rodriguez C, Boiardt H, Bolooki S, CubeSat to commercial intersatellite communications: past, present and future, Proceedings of the 2016 IEEE Aerospace Conference, Big Sky, MT, 5-12 Mar 2016.
  17. Song H, Park J, Buchert S, Jin Y, Chao CK, et al., A small peak in the swarm-Lp plasma density data at the dayside dip equator, J. Geophys. Res. Space Phys. 127, e2022JA030319 (2022). https://doi.org/10.1029/2022JA030319
  18. Song H, Park J, Lee J, Magnetometer calibration based on the CHAOS-7 model, J. Astron. Space Sci. 38, 157-164 (2021a). https://doi.org/10.5140/JASS.2021.38.3.157
  19. Song Y, Park SY, Lee S, Kim P, Lee E, et al., Spacecraft formation flying system design and controls for four nanosats mission, Acta Astronaut. 186, 148-163 (2021b). https://doi.org/10.1016/j.actaastro.2021.05.013
  20. Sohn J, Lee J, Jo G, Lee J, Hwang J, et al., Conceptual design of a solid state telescope for small scale magNetospheric ionospheric plasma experiments, J. Astron. Space Sci. 35, 195-200 (2018). https://doi.org/10.5140/JASS.2018.35.3.195