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International Applied Mechanics

, Volume 42, Issue 8, pp 959–965 | Cite as

On the dynamics of deployment of an orbital structure with elastic elements

  • V. I. Dranovskii
  • A. E. Zakrzhevskii
  • A. P. Kovalenko
  • V. S. Khoroshilov
Article

Abstract

The object to be studied is a spacecraft with a deployable pantograph structure as a solar-battery carrier. The objective of research is to design a mathematical model of this structure taking the elasticity of pantograph elements into account. The Lagrangian formalism is followed. To model the dynamic processes in the system, a software package has been developed, which can be adapted, if necessary, to study deployable structures of other types. The behavior of the structure during deployment, collapse, and redeployment under the action of various perturbations is modeled numerically. Plots illustrating the variation of characteristic variables are presented

Keywords

spacecraft solar batteries pantograph gravity-gradient boom deployment 

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References

  1. 1.
    V. I. Gulyaev, “Complex motion of elastic systems,” Int. Appl. Mech., 39, No. 5, 525–545 (2003).CrossRefGoogle Scholar
  2. 2.
    V. I. Gulyaev, V. V. Gaidaichuk, and A. G. Chernyavskii, “Dynamic behavior of a large deployable reflector,” Int. Appl. Mech., 39, No. 9, 1084–1088 (2003).CrossRefGoogle Scholar
  3. 3.
    L. H. Donnell, Beams, Plates, and Shells, McGraw Hill, New York (1976).MATHGoogle Scholar
  4. 4.
    V. I. Dranovskii, A. E. Zakrzhevskii, and V. S. Khoroshilov, “Dynamics of a program-reconfigurable spatial system of bodies,” Kosmich. Nauka Tekhnol., 10, No. 1, 45–53 (2004).ADSGoogle Scholar
  5. 5.
    A. E. Zakrzhevskii, “Optimal slewing of a flexible spacecraft,” Int. Appl. Mech., 39, No. 10, 1208–1214 (2003).CrossRefGoogle Scholar
  6. 6.
    G. S. Pisarenko, A. P. Yakovlev, and V. V. Matveev, Strength of Materials: Handbook [in Russian], Naukova Dumka, Kyiv (1988).Google Scholar
  7. 7.
    A. I. Lurie, Analytical Mechanics, Springer, Berlin-New York (2002).MATHGoogle Scholar
  8. 8.
    V. I. Gulyaev and S. N. Khudolii, “Vibrations of curved and twisted blades during complex rotation,” Int. Appl. Mech., 41, No. 4, 449–454 (2005).CrossRefGoogle Scholar
  9. 9.
    V. I. Gulyaev and M. Nabil, “Resonant interaction of a beam and an elastic foundation during the motion of a periodic system of concentrated loads,” Int. Appl. Mech., 41, No. 5, 560–565 (2005).CrossRefGoogle Scholar
  10. 10.
    S. N. Konyukhov, “Applied mechanics problems accompanying spacecraft launches from a floating platform and their resolution by the Sea Launch Project,” Int. Appl. Mech., 40, No. 2, 115–139 (2004).CrossRefGoogle Scholar
  11. 11.
    A. E. Zakrzevskii, I. Matarazzo, and V. S. Khoroshilov, “Dynamics of a system of bodies with program-variable configuration,” Int. Appl. Mech., 40, No. 3, 345–350 (2004).CrossRefGoogle Scholar

Copyright information

© Springer Science+Business Media, Inc. 2006

Authors and Affiliations

  • V. I. Dranovskii
    • 1
  • A. E. Zakrzhevskii
    • 2
  • A. P. Kovalenko
    • 2
  • V. S. Khoroshilov
    • 1
  1. 1.M. K. Yangel’ State Design Office “Yuzhnoe,”DnepropetrovskUkraine
  2. 2.S. P. Timoshenko Institute of MechanicsNational Academy of Sciences of UkraineKiev

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