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반작용휠과 제어모멘트자이로를 이용한 위성 고기동 연구

A Study on High Agile Satellite Maneuver using Reaction Wheels and CMGs

  • Son, Jun-Won (Science & Technology Satellite Division, Korea Aerospace Research Institute) ;
  • Rhee, Seung-Wu (Science & Technology Satellite Division, Korea Aerospace Research Institute)
  • 투고 : 2012.07.02
  • 심사 : 2013.01.07
  • 발행 : 2013.02.01

초록

네 개의 반작용휠과 두 개의 제어모멘트자이로를 이용하여 2축 고기동을 포함한 3축 자세제어방법을 연구하였다. 두 개의 제어모멘트자이로 때문에 발생하는 특이점에 대해 살펴보고 특이점을 탈출하는 방법을 제안하였다. 이 결과를 토대로 고기동을 위한 구동기 제어방법을 제안하였다. 아울러 자세제어 전후의 반작용휠과 제어모멘트자이로의 모멘텀이 유지되도록 하는 구동기 모멘텀 관리방법도 제안하였다. 시뮬레이션을 통하여 설계된 제어기법이 위성의 3축 제어 및 2축에 대한 고기동을 달성하며 구동기의 모멘텀도 보전하는 것을 확인하였다.

We study three axis attitude control method including two axis high agile maneuver using four reaction wheels and two control moment gyros. We investigate singularity conditions due to two control moment gyros and propose singularity escape method. Based on this, we propose actuator control algorithm for high agile maneuver. Also, we propose actuator momentum management method which preserves momentum of reaction wheels and control moment gyroscopes before and after satellite attitude control. Through numerical simulation, we show that our method achieves three axis attitude control including two axis high agile maneuver and preserves actuators' momentum.

키워드

참고문헌

  1. Lee, S.-H., "Technology of Control Moment Gyroscope and its Industrial Trend," Journal of The Korean Society for Aeronautical and Space Siences, Vol. 40, No. 1, 2012, pp. 86-92. https://doi.org/10.5139/JKSAS.2012.40.1.86
  2. Roser, X., and Sghedoni, M., "Control Moment Gyroscopes (CGM's) and Their Application in Future Scientific Missions," Proceedings of the 3rd ESA International Conference, Nov. 1996, pp. 523-528.
  3. Defendini, A., Lagadec, K., Guay, P., Blais, T., and Griseri, G., "Low cost CMG-Based AOCS Designs," Proceedings of the 4th ESA International Conference on Spacecraft Guidance, Navigation and Control Systems, Oct. 1999, pp. 393-398.
  4. Lappas, V. J., Steyn WH, and Underwood C. I., "Attitude Control for Small Satellite Using Control Moment Gyros," Acta Automacica, Vol. 51, 2002, pp. 101-111.
  5. Lappas, V., Oosthuizen, P., Madle, P, Cowie, L., Yuksel, G., and Fertin, D., "Micro CMGs for Agile Small Satellites: Design and In-Orbit Tests," Proceedings of the 6th International ESA Conference on Guidance, Navigation and Control Systems, Oct. 2005, pp.53.1.
  6. Asghar, S., Palmer, P.L., and Roberts, M., "An Exact Steering Law for Twin Control Moment Gyro Systems," Proceedings of the 6th ESA International Conference on Guidance, Navigation and Control Systems, Oct. 2005, pp.24.1.
  7. Lee, B., Oh, H., Kang, J., "Asymptotic Reduced-Dimensional Steering Strategies for CMG Singularity-Free Control," Journal of Mechanical Science and Technology, Vol. 21, No. 3, 2007, pp. 436-447. https://doi.org/10.1007/BF02916305
  8. Leeghim, H., Lee, I.H., Lee, D.H., Bang, H.C., and Park, J.O., "Singularity Avoidance of control Moment Gyros by Predicted Singularity Robustness: Ground Experiment," IEEE Transactions on Control Systems Technology, Vol. 17, No. 4, Jul, 2009, pp.884-891. https://doi.org/10.1109/TCST.2008.2011556
  9. Myung, H., Lee, H., Park, J., Bang, H., Oh, S.-H., and Yong, K.-L., "Analytic Moedling of Control Moment Gyros," Journal of The Korean Society for Aeronautical and Space Siences, Vol. 35, No. 7, 2007, pp. 640-646. https://doi.org/10.5139/JKSAS.2007.35.7.640
  10. Jin, J., "Analysis of Attitude Control Characteristics for an Underactuated Spacecraft Using a Single-Gimbal Varibale-Speed CMG," Journal of The Korean Society for Aeronautical and Space Siences, Vol. 38, No. 5, 2010, pp. 437-444. https://doi.org/10.5139/JKSAS.2010.38.5.437
  11. Seo, H.-H., Rhee, S.-W., Lee, S.-H., Oh, S.-H., Yim, J.-R, and Yong, K.-L., "Design Criteria and Cluster Configuration Improvement of Single Gimbal Control Moment Gyros for Satellite," Journal of The Korean Society for Aeronautical and Space Siences, Vol. 36, No. 1, 2008, pp. 48-56. https://doi.org/10.5139/JKSAS.2008.36.1.048
  12. Jang, W.-Y., Rhee, S.-W., and Kwon, H.-J., "Development of 0.6Nm Small CMG Hardware and Performance Test," Journal of The Korean Society for Aeronautical and Space Siences, Vol. 38, No. 9, 2010, pp. 933-942. https://doi.org/10.5139/JKSAS.2010.38.9.933
  13. Jang, W.-Y.,"Development of SGCMG for Small Satellite and Study on the Pratical Approach of SGCMG for Attitude Control," Master Thesis, University of Science and Technology, 2010.
  14. Lee, D., and Bang, H., "Time and Energy Optimal Spacecraft Attitude Trajectory using a CMG cluster," 2010 Fall Conference of The Korean Society for Aeuronautical and Space Sciences, Vol. II, 2010, pp. 866-869.
  15. Kwon, H.-J. and Rhee, S.-W., "CMGs Torque Measurement Test and Drift Removal Method," 2011 Spring Conference of The Korean Society for Aeuronautical and Space Sciences, 2011, pp. 1058-1061.
  16. Rhee, S.-W., and Kwon, H.-J., "Low Cost Small CMG Performance Test and Analysis," Journal of The Korean Society for Aeronautical and Space Siences, Vol. 39, No. 6, 2011, pp. 543-552. https://doi.org/10.5139/JKSAS.2011.39.6.543
  17. Son, J.-W., and Rhee, S.-W., "Satellite Attitude Control using Reaction Wheels and CMGs," Journal of The Korean Society for Aeronautical and Space Siences, Vol. 39, No. 10, 2011, pp. 935-945. https://doi.org/10.5139/JKSAS.2011.39.10.935