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Two-Blade Solar Sail Dynamics

  • Vera MayorovaEmail author
  • Alexander Popov
  • Nikolay Nerovnyy
  • Dmitry Rachkin
  • Stepan Tenenbaum
Chapter
Part of the Springer Praxis Books book series (PRAXIS)

Abstract

This paper is about research of dynamics of spatial motion of two-blade heliogyro solar sail considering different types of perturbing effects with their responsiveness and range. The main purpose of this work is determination of list of design objectives and their range to provide sustainable movement of picosatellite with two-blade solar sail in experiment BMSTU-Sail.

Keywords

Nominal Position Inertia Tensor Spherical Joint Solar Sail Angular Velocity Vector 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

  1. 1.
    Mayorova, V. I., Dmitriev A., Nerovnyy N., Rachkin D., Tenenbaum S., “ISS - test bed for the future solar sail systems”, 63 rd International Astronautical Congress, IAC-12-B3.3.10, Naples, Italy, 2012.Google Scholar
  2. 2.
    Weisstein, Eric W. “Monte Carlo Method.” From MathWorld-A Wolfram Web Resource. http://mathworld.wolfram.com/MonteCarloMethod.html [cited 10 May 2013].

Copyright information

© Springer-Verlag Berlin Heidelberg 2014

Authors and Affiliations

  • Vera Mayorova
    • 1
    Email author
  • Alexander Popov
    • 2
  • Nikolay Nerovnyy
    • 3
  • Dmitry Rachkin
    • 4
  • Stepan Tenenbaum
    • 4
  1. 1.Professor, Rocket Engineering and SpacecraftsBauman Moscow State Technical UniversityMoscowRussia
  2. 2.Assistant Professor, Aerospace SystemsBauman Moscow State Technical UniversityMoscowRussia
  3. 3.Engineer, Rocket Engineering and SpacecraftsBauman Moscow State Technical UniversityMoscowRussia
  4. 4.PhD Student, Aerospace SystemsBauman Moscow State Technical UniversityMoscowRussia

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