A fuel balancing method for reconfiguration of satellite formation flying

Sung Moon Yoo, Sang Young Park, Kyu Hong Choi

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

This paper presents a fuel balancing method for reconfiguration maneuvers of satellite formation flying based upon the circular Hill's problem. With the previous general analytic solution to optimal reconfiguration of satellite formation flying, an optimal starting phase angle for a formation reconfiguration maneuver is analytically calculated to keep fuel balance between deputy satellites. Using this optimal starting phase angle, we can estimate the period of maneuver for reconfiguration that yields fuel balancing.

Original languageEnglish
Title of host publicationICCAS 2007 - International Conference on Control, Automation and Systems
Pages1426-1429
Number of pages4
DOIs
Publication statusPublished - 2007 Dec 1
EventInternational Conference on Control, Automation and Systems, ICCAS 2007 - Seoul, Korea, Republic of
Duration: 2007 Oct 172007 Oct 20

Other

OtherInternational Conference on Control, Automation and Systems, ICCAS 2007
CountryKorea, Republic of
CitySeoul
Period07/10/1707/10/20

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All Science Journal Classification (ASJC) codes

  • Control and Systems Engineering
  • Electrical and Electronic Engineering

Cite this

Yoo, S. M., Park, S. Y., & Choi, K. H. (2007). A fuel balancing method for reconfiguration of satellite formation flying. In ICCAS 2007 - International Conference on Control, Automation and Systems (pp. 1426-1429). [4406562] https://doi.org/10.1109/ICCAS.2007.4406562
Yoo, Sung Moon ; Park, Sang Young ; Choi, Kyu Hong. / A fuel balancing method for reconfiguration of satellite formation flying. ICCAS 2007 - International Conference on Control, Automation and Systems. 2007. pp. 1426-1429
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Yoo, SM, Park, SY & Choi, KH 2007, A fuel balancing method for reconfiguration of satellite formation flying. in ICCAS 2007 - International Conference on Control, Automation and Systems., 4406562, pp. 1426-1429, International Conference on Control, Automation and Systems, ICCAS 2007, Seoul, Korea, Republic of, 07/10/17. https://doi.org/10.1109/ICCAS.2007.4406562

A fuel balancing method for reconfiguration of satellite formation flying. / Yoo, Sung Moon; Park, Sang Young; Choi, Kyu Hong.

ICCAS 2007 - International Conference on Control, Automation and Systems. 2007. p. 1426-1429 4406562.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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AB - This paper presents a fuel balancing method for reconfiguration maneuvers of satellite formation flying based upon the circular Hill's problem. With the previous general analytic solution to optimal reconfiguration of satellite formation flying, an optimal starting phase angle for a formation reconfiguration maneuver is analytically calculated to keep fuel balance between deputy satellites. Using this optimal starting phase angle, we can estimate the period of maneuver for reconfiguration that yields fuel balancing.

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Yoo SM, Park SY, Choi KH. A fuel balancing method for reconfiguration of satellite formation flying. In ICCAS 2007 - International Conference on Control, Automation and Systems. 2007. p. 1426-1429. 4406562 https://doi.org/10.1109/ICCAS.2007.4406562