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Applications in the Flight Attitude Control System

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Non-driven Micromechanical Gyroscopes and Their Applications

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Abstract

Due to the breakthrough provided by the calculation method and software, the output of multi-information from a “non-driven structure silicon micromechanical gyroscope” can be realized.

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Authors and Affiliations

  1. Beijing Information Science and Technology University, Beijing, China

    Fuxue Zhang & Wei Zhang

  2. Academy of Armored Forces Engineering, Beijing, China

    Guosheng Wang

Authors
  1. Fuxue Zhang
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  2. Wei Zhang
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  3. Guosheng Wang
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Corresponding author

Correspondence to Fuxue Zhang .

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© 2018 National Defense Industry Press and Springer-Verlag GmbH Germany

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Cite this chapter

Zhang, F., Zhang, W., Wang, G. (2018). Applications in the Flight Attitude Control System. In: Non-driven Micromechanical Gyroscopes and Their Applications. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-54045-9_11

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  • DOI: https://doi.org/10.1007/978-3-662-54045-9_11

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-662-54043-5

  • Online ISBN: 978-3-662-54045-9

  • eBook Packages: Physics and AstronomyPhysics and Astronomy (R0)

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