Location via proxy:   [ UP ]  
[Report a bug]   [Manage cookies]                
Skip to main content
Springer Nature Link
Log in

Fuzzy Knowledge Based Guidance in the Homing Missiles

  • Conference paper
Knowledge-Based Intelligent Information and Engineering Systems (KES 2003)

Part of the book series: Lecture Notes in Computer Science ((LNAI,volume 2773))

  • 966 Accesses

Abstract

A fuzzy knowledge based tail pursuit guidance scheme is proposed as an alternative to the conventional methods. The purpose of this method is to perform the tracking and interception using a simplified guidance law based on the fuzzy controller. Noise effects in homing missile guidance must be reduced to get an accurate control. In this work, developed fuzzy tail pursuit control algorithm reduces the noise effects. Then, a knowledge based algorithm is derived from the fuzzy control behavior to obtain a simplified guidance law. Simulation results show that the new algorithm led to satisfactory performance for the purpose of this work.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Log in via an institution

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

Similar content being viewed by others

References

  1. Lee, C.C.: Fuzzy Logic in Control Systems: Fuzzy Logic Controller: Part I & Part II. IEEE Trans. Syst. Man and Cybernetics 20, 404–435 (1990)

    Article  MATH  Google Scholar 

  2. Williams, T.: Fuzzy Logic Simplifies Complex Control Problems. Computer Design, 90–102 (1991)

    Google Scholar 

  3. Huang, C., Tylock, J., Engel, S., Whitson, J.: Comparison of Neural Network Based, Fuzzy Logic Based, and Numerical Nonlinear Inverse Flight Control. In: Proceedings of the AIAA Guidance, Navigation and Control Conference, AIAA Washington DC, pp. 922–929 (1994)

    Google Scholar 

  4. Geng, Z.J., McCullough, C.L.: Missile Control Using Fuzzy Cerebellar Model Arithmetic Computer Neural Networks. Journal of Guidance, Control and Dynamics 20(3), 557–565 (1997)

    Article  MATH  Google Scholar 

  5. Lin, C.L., Chen, Y.Y.: Design of an Advanced Guidance Law Against High Speed Attacking Target. In: Proceedings of the National Science Council, Part A, vol. 23(1), pp. 60–74 (1999)

    Google Scholar 

  6. Mishra, K., Sarma, I.G., Swamy, K.N.: Performance Evaluation of the Fuzzy Logic Based Homing Guidance Schemes. Journal of Guidance, Control and Dynamics 17(6), 1389–1391 (1994)

    Article  Google Scholar 

  7. Gonsalves, P.G., Çağlayan, A.K.: Fuzzy Logic PID Controller for Missile Terminal Guidance. In: Proceedings of 1995 IEEE International Symposium and Intelligent Control, pp. 377–382. IEEE Publications, Piscataway (1995)

    Google Scholar 

  8. Lin, C.L., Chen, Y.Y.: Design of Fuzzy Logic Guidance Law Against High Speed Target. Journal of Guidance, Control and Dynamics 23(1), 17–25 (2000)

    Article  Google Scholar 

  9. Hoang, L.H., Maher, H.: Control of a Direct-Drive DC Motor by Fuzzy Logic. IEEE Industry Applications Society VI, 732–738 (1993)

    Google Scholar 

Download references

Author information

Authors and Affiliations

  1. System Dynamics and Control Unit, Mechanical Engineering Faculty, Istanbul Technical University, Turkey

    Mustafa Resa Becan & Ahmet Kuzucu

Authors
  1. Mustafa Resa Becan
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. Ahmet Kuzucu
    View author publications

    You can also search for this author in PubMed Google Scholar

Editor information

Editors and Affiliations

  1. Computing Laboratory, Oxford University, Parks Road, OXI 3QD, United Kingdom

    Vasile Palade

  2. Intelligent Systems and Signal Processing Labs, Moulsecoomb, University of Brighton, BN2 4GJ, Brighton, United Kingdom

    Robert J. Howlett

  3. Knowledge-Based Intelligent Engineering Systems Centre, Mawson Lakes, University of South Australia, 5095, Adelaide, SA, Australia

    Lakhmi Jain

Rights and permissions

Reprints and permissions

Copyright information

© 2003 Springer-Verlag Berlin Heidelberg

About this paper

Cite this paper

Becan, M.R., Kuzucu, A. (2003). Fuzzy Knowledge Based Guidance in the Homing Missiles. In: Palade, V., Howlett, R.J., Jain, L. (eds) Knowledge-Based Intelligent Information and Engineering Systems. KES 2003. Lecture Notes in Computer Science(), vol 2773. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-45224-9_36

Download citation

  • DOI: https://doi.org/10.1007/978-3-540-45224-9_36

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-40803-1

  • Online ISBN: 978-3-540-45224-9

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics

Search

Navigation