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LPV Modeling of the Missile Attitude Control System Based on Small Deviation Equation

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Electrical, Information Engineering and Mechatronics 2011

Part of the book series: Lecture Notes in Electrical Engineering ((LNEE,volume 138))

Abstract

With a concern about the missile attitude control system, this paper attempts to solve the online calculation method of the coefficient of the small deviation equation, on which a LFT-based LPV model of the missile attitude control system is set up.

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References

  1. Shamma JS, Athans M (1990) Analysis of nonlinear gain-scheduled control systems. IEEE Trans Autom Control 35:898–907

    Article  MathSciNet  MATH  Google Scholar 

  2. Shamma JS, Athans M (1991) Guaranteed properties of gain scheduled control for linear parameter-varying plants. Automatica 27:559–564

    Article  MathSciNet  MATH  Google Scholar 

  3. Packard A (1994) Gain scheduling via linear fractional transformations. Syst Cont Lett 22:79–92

    Article  MathSciNet  MATH  Google Scholar 

  4. Apkarian P, Gahinet P (1995) A convex characterization of gain-scheduled \( H_{\infty } \) controllers. IEEE Tran Autom Cont 40:853–864

    Google Scholar 

  5. Becker G, Packard A (1994) Robust performance of linear parametrically varying systems using parametrically-dependent linear feedback. Syst Cont Lett 23:205–215

    Article  MathSciNet  MATH  Google Scholar 

  6. Becker G (1996) Additional results on parameter-dependent controllers for LPV systems. In: Proceedings of the 13th IFAC world congress, pp 351–356

    Google Scholar 

  7. Wu F, Yang XH, Packard A, Becker G, Induced \( L_{2} \) norm control for LPV systems with bounded parameter variation rates. Int J Rob Non Cont 6:983–998

    Google Scholar 

  8. Yu J, Sideris A (1997) \( H_{\infty } \) control with parametric Lyapunov functions. Syst Cont Lett 30:57–69

    Google Scholar 

  9. Apkarian P, Adams R (1998) Advanced gain scheduling techniques for uncertain system. IEEE Trans Cont Syst Technol 6:21–32

    Article  Google Scholar 

  10. Xu Y (1999) Design and analysis of the control system of the ballistic missile and launch vehicle. Aerospace Press, Auburn

    Google Scholar 

  11. Xu Y (1989) Control system. Aerospace Press, Auburn

    Google Scholar 

  12. Guo Di, Rugh WJ (1995) A stability result for linear parameter-varying systems. Syst Cont Lett 24:1–5

    Article  MathSciNet  MATH  Google Scholar 

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Acknowledgments

This work was supported in part by the National Nature Science Foundation of China, No 60975058, Nature Science Foundation of Hubei NO.2010CDB01904, 2010 Aerospace Technology Support Foundation, 2010 Defense Innovation Research Foundation of Huazhong University of Science and Technology.

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Correspondence to Lei Liu .

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© 2012 Springer-Verlag London Limited

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Ni, S., Wu, J., Shan, J., Liu, L., Wang, Y., Hu, K. (2012). LPV Modeling of the Missile Attitude Control System Based on Small Deviation Equation. In: Wang, X., Wang, F., Zhong, S. (eds) Electrical, Information Engineering and Mechatronics 2011. Lecture Notes in Electrical Engineering, vol 138. Springer, London. https://doi.org/10.1007/978-1-4471-2467-2_218

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  • DOI: https://doi.org/10.1007/978-1-4471-2467-2_218

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  • Publisher Name: Springer, London

  • Print ISBN: 978-1-4471-2466-5

  • Online ISBN: 978-1-4471-2467-2

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