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Authors
Abedi, Mostafa; Bolandi, Hossein; Saberi, Farhad Fani

Digital Object Identifier (DOI)
10.3182/20070625-5-FR-2916.00011

Page Numbers:
55-60

Index Terms
guidance,missile,adaptive,Takagi-Sugeno,fuzzy,target,uncertainty,robust

Abstract
This paper proposes an observer based adaptive Takagi-Sugeno fuzzy guidance law for a surface to air missile. An integrated guidance-control model is derived to consider target manoeuvre and missile uncertainties in the design process of the proposed guidance law, also use of adaptive intelligent system for approximation of unknown dynamic parts of the mentioned model and a high gain observer for estimation of required states caused that this approach, in contrast to guidance approaches introduced by now, use the minimum number of inputs for a robust missile guidance. Presented proofs and simulated results show the practical application and effective performance of designed guidance law.

References

[1] Blackelock J. H. (1991). Automatic Control of
    Aircraft and Missiles. pp. 229-259. John Wiley,
    New York.
[2] Chaw D. and J. Y. Choi (2002). New parametric
    Affine Modelling and Control for Skid-to-Turn
    Missiles. IEEE Transaction on Control Systems
    Technology, vol. 9, no. 2, pp. 335-347.
[3] Chaw D. and J. Y. Choi (2003). Adaptive Nonlinear
    Guidance Law Considering Control Loop
    Dynamics. IEEE Transaction on Aerospace and
    Electronic Systems, vol. 39, no. 4, pp. 1134-
    1143.
[4] Ghose D. (1994). True Proportional Navigation with
    Manoeuvring Target. IEEE Transaction on
    Aerospace and Electronic Systems, vol. 30, no
    1, pp. 229-237.
[5] Ke F.. (2003). Design of Optimal Midcourse
    Guidance Sliding-Mode Control for Missiles
    with TVC. IEEE Transaction on Aerospace and
    Electronic Systems, vol. 39, no. 3, pp. 824-837.
[6] Khalil H. K. (1993). Asymptotic Regulation of
    Minimum Phase Nonlinear Systems Using
    Output Feedback. in Processing of American
    Control Conference, San Francisco, CA, pp.
    1490-1494.
[7] Mahapatra P. R. and U. S. Shukla (1989). Accurate
    Solution of Proportional Navigation for
    Manoeuvring Targets. IEEE Transaction on
    Aerospace and Electronic Systems, vol. AES-
    25, no. 1, pp. 81-89.
[8] Swaroop D., J. K. Hedrick, P. P. Yip, and J. C.
    Gerdes (2000). Dynamic Surface Control for a
    Class of Nonlinear Systems. IEEE Transaction
    on Automatic Control, vol. 45, no. 10, pp. 1893-
    1899.
[9] Wang, C. H., H. L. Liu and T. C. Lin (2002). Direct
    Adaptive Fuzzy-Neural Control with State
    Observer and Supervisory Controller for
    Unknown Nonlinear Dynamical Systems. IEEE
    Transaction on Fuzzy Systems, vol. 10, no. 1,
    pp. 39-49.