Integral Global Sliding Mode Guidance for Impact Angle Control

Shaoming He; Defu Lin; Jiang Wang

doi:10.1109/TAES.2018.2876588

Integral Global Sliding Mode Guidance for Impact Angle Control

Shaoming He, Defu Lin, Jiang Wang^*

^*Corresponding author for this work

School of Aerospace Engineering

Cranfield University

Research output: Contribution to journal › Article › peer-review

36 Citations (Scopus)

Abstract

This paper proposes a new guidance law based on integral sliding mode control (ISMC) technique for maneuvering target interception with impact angle constraint. A time-varying function weighted line-of-sight error dynamics, representing the nominal guidance performance, is introduced first. The proposed guidance law is derived by utilizing ISMC to follow the desired error dynamics. The convergence of the guidance law developed is supported by Lyapunov stability. Simulations with extensive comparisons explicitly demonstrate the effectiveness of the proposed approach.

Original language	English
Pages (from-to)	1843-1849
Number of pages	7
Journal	IEEE Transactions on Aerospace and Electronic Systems
Volume	55
Issue number	4
DOIs	https://doi.org/10.1109/TAES.2018.2876588
Publication status	Published - 1 Aug 2019

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10.1109/TAES.2018.2876588

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title = "Integral Global Sliding Mode Guidance for Impact Angle Control",

abstract = "This paper proposes a new guidance law based on integral sliding mode control (ISMC) technique for maneuvering target interception with impact angle constraint. A time-varying function weighted line-of-sight error dynamics, representing the nominal guidance performance, is introduced first. The proposed guidance law is derived by utilizing ISMC to follow the desired error dynamics. The convergence of the guidance law developed is supported by Lyapunov stability. Simulations with extensive comparisons explicitly demonstrate the effectiveness of the proposed approach.",

author = "Shaoming He and Defu Lin and Jiang Wang",

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N2 - This paper proposes a new guidance law based on integral sliding mode control (ISMC) technique for maneuvering target interception with impact angle constraint. A time-varying function weighted line-of-sight error dynamics, representing the nominal guidance performance, is introduced first. The proposed guidance law is derived by utilizing ISMC to follow the desired error dynamics. The convergence of the guidance law developed is supported by Lyapunov stability. Simulations with extensive comparisons explicitly demonstrate the effectiveness of the proposed approach.

AB - This paper proposes a new guidance law based on integral sliding mode control (ISMC) technique for maneuvering target interception with impact angle constraint. A time-varying function weighted line-of-sight error dynamics, representing the nominal guidance performance, is introduced first. The proposed guidance law is derived by utilizing ISMC to follow the desired error dynamics. The convergence of the guidance law developed is supported by Lyapunov stability. Simulations with extensive comparisons explicitly demonstrate the effectiveness of the proposed approach.

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Integral Global Sliding Mode Guidance for Impact Angle Control

Abstract

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