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SMC for Missile Systems Based on Back-Stepping and ESO Techniques

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Compound Control Methodology for Flight Vehicles

Part of the book series: Lecture Notes in Control and Information Sciences ((LNCIS,volume 438))

Abstract

There have been a great many researches on control designs for missiles with highly nonlinear characteristics using nonlinear control techniques [26, 134, 142, 183, 206, 291]. Back-stepping control design is one of the nonlinear feedback methods for controlling nonlinear systems. It is based on Lyapunov theory and capable of solving complicated nonlinear systems. The back-stepping method makes the design of the feedback control strategy systematic: it consists of a recursive determination of a virtual Lyapunov-based control signal and obtaining the actual control law up to the last step. With this characteristic, the back-stepping technique is more flexible in designing controllers for high-order nonlinear system models. In the last decade, back-stepping theory has been widely used to solve the transient stabilization problems in missile and flight systems [115, 67, 131, 228].

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Correspondence to Yuanqing Xia .

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Xia, Y., Fu, M. (2013). SMC for Missile Systems Based on Back-Stepping and ESO Techniques. In: Compound Control Methodology for Flight Vehicles. Lecture Notes in Control and Information Sciences, vol 438. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-36841-7_5

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  • DOI: https://doi.org/10.1007/978-3-642-36841-7_5

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-36840-0

  • Online ISBN: 978-3-642-36841-7

  • eBook Packages: EngineeringEngineering (R0)

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