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Research on Attitude Law of Mass Moment Missile

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Book cover Fuzzy Systems and Knowledge Discovery (FSKD 2006)

Part of the book series: Lecture Notes in Computer Science ((LNAI,volume 4223))

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Abstract

The ability of moving mass attitude control is investigated for mass moment missile with three-axial stabilization. On basis of constructing the attitude model of mass moment missile with three moving masses, the coupled influence to this system is described which is caused by the relative movement between the moving masses and the cartridge case. Then an attitude control law based on fuzzy logic is presented for the mass moment missile and the fuzzy rule tables corresponding to the moving mass position in respective axial are constituted. According to analysis of the relation between angular acceleration and searching condition, three moving mass positions are regulated in phase. Simulation results show that the system stabilization can be satisfied to realize efficiently attitude adjustment for missile.

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References

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Author information

Authors and Affiliations

  1. Control & Simulation Center, Harbin Institute of Technology, 150001, Harbin, P.R. China

    Qing Guo, Ming Yang & Zi-cai Wang

Authors
  1. Qing Guo
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  2. Ming Yang
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  3. Zi-cai Wang
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Editor information

Editors and Affiliations

  1. School of Electrical and Electronic Engineering, Nanyang Technological University,, Block S1, Nanyang Avenue, 639798, Singapore

    Lipo Wang

  2. Life Science Research Center, School of Electronic Engineering, Xidian University,, 710071, Xi’an, Shaanxi, China

    Licheng Jiao

  3. School of Electrical and Electronic Engineering, Xidian University, 710071, Xi’an, China

    Guanming Shi

  4. School of Information Technology and Electrical Engineering, The University of Queensland, 4072, Brisbane, Queensland, Australia

    Xue Li

  5. College of Mathematics and Information Science, Hebei Normal University, 050016, Shijiazhuang, Hebei, P.R. China

    Jing Liu

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© 2006 Springer-Verlag Berlin Heidelberg

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Guo, Q., Yang, M., Wang, Zc. (2006). Research on Attitude Law of Mass Moment Missile. In: Wang, L., Jiao, L., Shi, G., Li, X., Liu, J. (eds) Fuzzy Systems and Knowledge Discovery. FSKD 2006. Lecture Notes in Computer Science(), vol 4223. Springer, Berlin, Heidelberg. https://doi.org/10.1007/11881599_105

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  • DOI: https://doi.org/10.1007/11881599_105

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-45916-3

  • Online ISBN: 978-3-540-45917-0

  • eBook Packages: Computer ScienceComputer Science (R0)

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