Russian Aeronautics

, Volume 61, Issue 1, pp 23–31 | Cite as

Parametric Identification of a Return Space Vehicle during Vertical Landing

  • V. A. Afanas’ev
  • G. L. Degtyarev
  • A. S. MeshchanovEmail author
Flight Dynamics and Control of Flight Vehicles


Real values of parameters for a space vehicle and its steering devices are specified by using the motion parameters measured in flight based on solving the differential equations of motion.


space vehicle vertical fall thrust vertical landing identification of parameters by altitude and velocity 


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Copyright information

© Allerton Press, Inc. 2018

Authors and Affiliations

  • V. A. Afanas’ev
    • 1
  • G. L. Degtyarev
    • 2
  • A. S. Meshchanov
    • 2
    Email author
  1. 1.South Ural State University (National Research University)MiassRussia
  2. 2.Tupolev Kazan National Research Technical UniversityKazan TatarstanRussia

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