Journal of the Korean Society for Aeronautical & Space Sciences (한국항공우주학회지)

The Korean Society for Aeronautical and Space Sciences (한국항공우주학회)
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Five Reaction Wheel Operation Method for Active SAR Satellite

능동 합성개구레이더위성의 다섯 개 반작용휠 운용방법

  • Received : 2016.05.27
  • Accepted : 2016.07.29
  • Published : 2016.09.01
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Abstract

For satellite attitude control and maneuver, normally four reaction wheels are used through pyramid configuration. However, if satellite's moment of inertia is large or available reaction wheels' capability is small, we can consider using five reaction wheels. In this case, we should think the arrangement of wheels and their operation method. Active SAR satellite requires high agile maneuver about roll axis to achieve looking angle change. In this research, we study the operation method of five reaction wheels configuration for fast roll maneuver.

위성의 자세제어 및 기동을 위해서는 네 개의 반작용휠을 피라미드 형태로 배치하여 사용하는 것이 일반적이다. 하지만 위성의 관성모멘트가 크거나 사용할 수 있는 반작용휠의 용량이 작은 경우에는 다섯 개의 반작용휠을 사용하는 것을 생각해볼 수 있다. 이 경우, 반작용휠 배치부터 운용방법까지 여러 가지 문제를 다시 고려해야 한다. 능동합성개구레이더 위성은 관측 각도 변화를 위해서 롤축 방향으로 빠른 기동이 요구된다. 본 논문에서는 합성개구레이더 위성의 롤축 방향 기동성능 향상을 위하여 다섯 개의 반작용휠을 배치하는 경우, 이를 운용하는 방법을 연구해본다.

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References

  1. Covello, F., Battazza,F., Coletta, A., Manoni, G., and Valentini, G. "Cosmo-skymed Mission Status: Three Out of Four Satellites in Orbit", IEEE International Geoscience and Remote Sensing Symposium, 2009, pp. 773-776.
  2. Werninghaus, R., and Buckreuss, S., "The TerraSar-X Mission and System Design", IEEE Trans. on Geoscience and Remote Sensing, Vol. 48, No. 2, 2010, pp. 606-614 https://doi.org/10.1109/TGRS.2009.2031062
  3. Rodriguez-Cassola, M. et. al, "First Bistatic Spaceborne SAR Experiments with TanDEM-X", IEEE Geoscience and Remote Sensing letters, Vol. 9, No., 1, 2012, pp. 33-37. https://doi.org/10.1109/LGRS.2011.2158984
  4. Arikawa, Y., Sarywatari, H., Hatooka, Y., and Suzuki, S., "ALOS-2 Launch and Early Orbit Operation Result", IEEE International GeoScience and Remote Sensing Symposium, 2014, pp. 3406-3409
  5. Lee, S.-Y., Kim, J.-H., and Yoon, J.-C.,"Development of KOMPSAT-5 System," Conference of the Korean Society for Aeronautical and Space Sciences, 2012 Fall, pp. 846-850.
  6. Oh, S.-H. Lee, S.-H., Yoon, S.-T., and Kim, J.-H., "Satellite Attitude Command Generation Minimizing the Doppler Centroid," Conference of the Korean Society for Aeronautical and Space Sciences, 2012, Spring, pp. 1059-1063.
  7. Son, J.-W., and Park, Y.-W., "A Study on Active SAR Satellite Maneuver Time Reduction through Sequential Rotation," Journal of the Korean Society for Aeronautical and Space Science, Vol. 43, No. 7, 2015, pp. 648-656 https://doi.org/10.5139/JKSAS.2015.43.7.648
  8. Yoon, H.-J., Seo, H.-H., and Choi, H.-T., "Optimal uses of reaction wheels in the pyramid configuration using a new minimum infinity-norm solution," Aerospace Science and Techonology, Vol. 39, 2014, pp. 109-119 https://doi.org/10.1016/j.ast.2014.09.002
  9. Park, Y.-W., and Choi, H.-T., "Study on the wheel allocation and the wheel momentum off-loading for COMS having asymmetric solar array configuration," Aerpsoace Engineering and Techonology, Vol. 12, No. 2, pp. 57-63
  10. Son, J.-W., Lee, S.-H., and Choi, H.-T., "Reaction Wheel Arrangement of 1-axis Highly Agile Satellite," Conference of the Korean Society for Aeronautical and Space Science, 2014, Autumn, pp. 563-567
  11. Son, J.-W., and Park, Y.-W., "Five Reaction Wheel Arrangement for 1-axis One Directional Highly Agile Satellite," Conference of the Korean Society for Aeronautical and Space Sciences, 2015, Autumn