Reliability Analysis of the Deployment of Astro-Mesh Antenna

  • Min-juan WangEmail author
  • Qi Yue
  • Jing Guo
Conference paper
Part of the Advances in Intelligent Systems and Computing book series (AISC, volume 891)


The deployment reliability of the Astro-Mesh of a large satellite antenna is investigated. By contrasting the difference of movement principium, a mechanical analysis model is presented. Considering the effects of the randomness of dimensional errors and the space environment factors, the failure models of two performance functions are established by means of the random functional movement method and the second moment method. The corresponding computational expressions for reliability analysis are derived by using the first order second moment method. Furthermore, the theoretical basis and reference are provided for the deployment reliability of a large satellite antenna, and some useful conclusions are obtained.


Satellite antenna Astro-Mesh antenna Random variable Reliability analysis 



This work was supported by the Department of Education Shaanxi Province, China, under Grant 2013JK1073.


  1. 1.
    Tibert, G.: Deployable Tensegrity Structures for Space Applications. Royal Institute of Technology, Stockholm (2002)Google Scholar
  2. 2.
    Tanaka, H.: Design optimization studies for large-scale contoured beam deployable satellite antennas. Acta Astronaut. 58(9), 443–451 (2006). Scholar
  3. 3.
    Vu, K.K., Liew, J.Y.R., Anandasivam, K.: Deployable tension-strut structures: from concept to implementation. J. Constr. Steel Res. 62(3), 195–209 (2006). Scholar
  4. 4.
    Werner, U.: Influence of electromagnetic field damping on forced vibrations of induction rotors caused by dynamic rotor eccentricity. J. Appl. Math. Mech. 97(1), 38–39 (2017). Scholar
  5. 5.
    Wettergren, J., Bonnedal, M., Ingvarson, P., Wästberg, B.: Antenna for precise orbit determination. Acta Astronaut. 65(11–12), 1765–1771 (2009). Scholar
  6. 6.
    Zhu, Z.-q., Chen, J.-j., Liu, G.-l., et al.: Reliability analysis for the deployment mechanism of a large satellite antenna based on unascertained information. J. Xidian Univ. 36(5), 909–915 (2009)Google Scholar
  7. 7.
    Patel, J., Ananthasuresh, G.K.: A kinematic theory for radially foldable planar linkages. Int. J. Solids Struct. 44(18), 6279–6298 (2007). Scholar
  8. 8.
    Lin, L., Chen, J., Liu, G., et al.: Fault analysis of deployment mechanism systems of satellite antennas based on the grey relation method. Chin. High Technol. Lett. 20(9), 905–910 (2010)Google Scholar
  9. 9.
    Omer Soykasap.: Analysis of tape spring hinges. Int. J. Mech. Sci. 49(2), 853–860 (2007). Scholar

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© Springer Nature Switzerland AG 2019

Authors and Affiliations

  1. 1.Xi’an University of Posts and TelecommunicationsXi’anChina

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