DOI QR코드

DOI QR Code

Microvibration analysis of a cantilever configured reaction wheel assembly

  • Zhang, Zhe (University of Southampton) ;
  • Aglietti, Guglielmo S. (Surrey Space Centre, University of Surrey) ;
  • Ren, Weijia (Chinese Academy of Sciences) ;
  • Addari, Daniele (Surrey Space Centre, University of Surrey)
  • Received : 2014.04.17
  • Accepted : 2014.05.08
  • Published : 2014.10.25

Abstract

This article discusses the microvibration analysis of a cantilever configured reaction wheel assembly. Disturbances induced by the reaction wheel assembly were measured using a previously designed platform. Modelling strategies for the effect of damping are presented. Sine-sweep tests are performed and a method is developed to model harmonic excitations based on the corresponding test results. The often ignored broadband noise is modelled by removing spikes identified in the raw signal including a method of identifying spikes from energy variation and band-stop filter design. The validation of the reaction wheel disturbance model with full excitations (harmonics and broadband noise) is presented and flaws due to missing broadband noise in conventional reaction wheel assembly microvibration analysis are discussed.

Keywords

References

  1. Aglietti, G.S., Langley, R.S., Rogers, E. and Gabriel, S.B. (2004), "Model building and verification for active control of microvibrations with probabilistic assessment of the effects of uncertainties", Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 218(4), 389-399.
  2. Bialke, B. (2011), "Microvibration disturbance fundamentals for rotating mechanisms", Proceedings of the 34th Annual Guidance and Control Conference, Breckenridge, CO.
  3. Bialke, B. (1996), "Microvibration disturbance sources in reaction wheels and momentum wheels", Proceedings of the European Conference on Spacecraft Structures, Materials & Mechanical Testing, Noordwijk, The Netherlands.
  4. Bialke, B. (1992), "A new family of low cost momentum/reaction wheels", Proceedings of the Annual AAS Guidance and Control Conference, Keystone, CO.
  5. Bosgra, J. and Prins, J.J.M. (1982), "Testing and investigation of reaction wheels", Proceedings of the Automatic Control in Space, 9th Symposium.
  6. ECSS-E-HB-32-26A, ECSS-E-HB-32-26A Spacecraft Mechanical Loads Analysis Handbook, ESA Requirements and Standards Division, ESA Requirements and Standards Division.
  7. Heimel, H. (2011), "Spacewheel microvibration - sources, appearance, countermeasures", Proceedings of the 8th Int'l ESA Conference on Guidance & Navigation Control Systems, Karlovy Vary, Czech Republic
  8. Kenney, H.B. (1963), "A Gryo momentum exchange device for space vehicle attitude control", AIAA J., 1(5), 1110-1118. https://doi.org/10.2514/3.1732
  9. Kim, D.K., Oh, S.H., Yong, K.L. and Yang, K.H. (2010), "Numerical study on a reaction wheel and wheeldisturbance modeling", J. Korean Soc. Aeronaut. Space Sci., 38(7), 702-708.
  10. Laurens, P. and Decoux, E. (1997a), "Microdynamic behaviour of momentum and reaction wheels", Proceedings of the Second Space Microdynamics and Accurate Symposium, Toulouse, Fracne.
  11. Laurens, P. and Decoux, E. (1997b), "Understanding and monitoring space mechanisms through their microdynamic signature", Proceedings of the 7th European Space Mechanisms and Tribology Symposium, Noordwijk, Netherlands.
  12. Liu, K.C., Maghami, P. and Blaurock, C. (2008), "Reaction wheel disturbance modeling, jitter analysis, and validation tests for solar dynamics observatory", Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit, Honolulu, Hawaii.
  13. Masterson, R.A., Miller, D.W. and Grogan, R.L. (2002), "Development and validation of reaction wheel disturbance models: empirical model", J. Sound Vib., 249(3), 575-598. https://doi.org/10.1006/jsvi.2001.3868
  14. Masterson, R.A., Miller, D.W. and Grogan, R.L. (1999), "Development of empirical and analytical reaction wheel disturbance models", Proceedings of the Structures, Structural Dynamics and Materials Conference, St. Louis, MO, USA.
  15. Miller, S.E., Kirchman, P. and Sudey, J. (2007), "Reaction wheel operational impacts on the GOES-N jitter environment", Proceedings of the AIAA Guidance, Navigation and Control Conference and Exhibit, South Carolina, USA.
  16. Seiler, R. and Allegranza, C. (2009), "Mechanism noise signatures: identification and modelling", Proceedings of the 14th European Space Mechanisms and Tribology Symposium, Vienna, Austria.
  17. Shin, Y.H., Heo, Y.H., Oh, S.H., Kim, D.K., Kim, K.J. and Yong, K.L. (2010), "Identification of input force for reaction wheel of satellite by measured action forceon decelerating", Tran. Korean Soc. Noise Vib. Eng., 20(3), 263-271. https://doi.org/10.5050/KSNVE.2010.20.3.263
  18. Takahara, O., Yoshida, N. and Minesugi, K. (2004), "Microvibration transmissibility test of solar-B", Proceedings of the 24th International Symposium on Space Technology and Science, Miyazaki, Japan
  19. Tan, A., Meurers, T., Veres, S., Aglietti, G. and Rogers, E. (2005), "Robust control of microvibrations with experimental verification", Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 219(5), 453-460. https://doi.org/10.1243/095440605X16929
  20. Toyoshima, M., Jono, T., Takahashi, N., Yamawaki, T., Nakagawa, K. and Arai, K. (2003), "Transfer functions of microvibrational disturbances on a satellite", Proceedings of the 21st International Communications Satellite Systems Conference and Exhibit, Yokohama, Japan
  21. Zhang, Z., Aglietti, G. and Ren, W. (2012a), "Microvibration model development and validation of a cantilevered reaction wheel assembly", Appl. Mech. Mater., 226-228, 133-137. https://doi.org/10.4028/www.scientific.net/AMM.226-228.133
  22. Zhang, Z., Aglietti, G. and Zhou, W. (2011), "Microvibrations induced by a cantilevered wheel assembly with a soft-suspension system", AIAA J., 49(5), 1067-1079. https://doi.org/10.2514/1.J050791
  23. Zhang, Z., Ren, W. and Aglietti, G. (2012b), "Coupled disturbance modelling and validation of a reaction wheel model", Proceedings of the European Conference on Spacecraft Structures, Materials & Environmental Testing, Noordwijk, The Netherlands.
  24. Zhang, Z., Aglietti, G.S. and Ren, W. (2013), "Coupled microvibration analysis of a reaction wheel assembly including gyroscopic effects in its accelerance", J. Sound Vib., 332(22), 5748-5765. https://doi.org/10.1016/j.jsv.2013.06.011
  25. Zhang, Z., Yang, L. and Pang, S. (2009), "Jitter environment analysis for micro-precision spacecraft", Spacecraft Envirom. Eng., 26(6), 528-534.
  26. Zhou, W.Y., Aglietti, G.S. and Zhang, Z. (2011), "Modelling and testing of a soft suspension design for a reaction/momentum wheel assembly", J. Sound Vib., 330(18-19), 4596-4610. https://doi.org/10.1016/j.jsv.2011.03.028

Cited by

  1. Dynamic Mass of a Reaction Wheel Including Gyroscopic Effects: An Experimental Approach vol.55, pp.1, 2017, https://doi.org/10.2514/1.J055398
  2. Experimental Validation of Fly-Wheel Passive Launch and On-Orbit Vibration Isolation System by Using a Superelastic SMA Mesh Washer Isolator vol.2017, 2017, https://doi.org/10.1155/2017/5496053