Abstract
Based on previous work, a Nussbaum gian controller is proposed to solve the unknown input direction problem of a large family of supersonic missiles. Also considering the one order dynamic characteristic of actuator , the uncertainties of nonlinear missile system, which is assumed to satisfy the so-called bounded uncertainty condition, are coped by the adopting of integral action and backstepping technology.And the unknown control direction problem of supersonic missile is solved by adopting of the Nussbaum gain method. A novel analysis with Lyapunov function and Nussbaum gain function are completed and the stability of the whole system is guaranteed by constructing of the Lyapunov function.
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References
Kim, S.-H., Kim, Y.-S., Song, C.: Contr. Eng. Prac. 12, 149–154 (2004)
Hull, R.A., Qu, Z.: Design and evaluation of robust nonlinear missile autopilot from a performance perspective. In: Proce. of the ACC, pp. 189–193 (1995)
Lei, J., Wang, X., Lei, Y.: How many parameters can be identified by adaptive synchronization in chaotic systems? Phys. Lett. A 373, 1249–1256 (2009)
Lei, J., Wang, X., Lei, Y.: A Nussbaum gain adaptive synchronization of a new hyperchaotic system with input uncertainties and unknown parameters. Commun. Nonlinear Sci. Numer. Simul. 14, 3439–3448 (2009)
Wang, X., Lei, J., Lei, Y.: Trigonometric RBF Neural Robust Controller Design for a Class of Nonlinear System with Linear Input Unmodeled Dynamics. Appl. Math. Comput. 185, 989–1002 (2007)
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© 2011 Springer-Verlag Berlin Heidelberg
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Wu, J., Lei, J., Gu, W., Shi, J. (2011). Adaptive Control of Supersonic Missiles with Unknown Input Coefficients. In: Lin, S., Huang, X. (eds) Advances in Computer Science, Environment, Ecoinformatics, and Education. CSEE 2011. Communications in Computer and Information Science, vol 214. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-23321-0_97
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DOI: https://doi.org/10.1007/978-3-642-23321-0_97
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-23320-3
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