Three-dimensional terminal angle constraint guidance law with class K∞ function-based adaptive sliding mode control

This paper investigates the three-dimensional (3-D) interception guidance problem, where the missile is required to intercept the maneuvering target with the desired terminal angles. For the nonlinear relative kinematic model, a class K∞ function-based adaptive sliding mode guidance law is proposed,...

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Bibliographic Details

Published in:	Aerospace science and technology Vol. 147; p. 109005
Main Authors:	Zheng, Zewei, Li, Jiazhe, Feroskhan, Mir
Format:	Journal Article
Language:	English
Published:	Elsevier Masson SAS 01-04-2024
Subjects:	Adaptive control Class [formula omitted] function Sliding mode control Terminal angle constraint Three-dimensional guidance law Three-dimensional guidance law Terminal angle constraint Adaptive control Sliding mode control Class K∞ function
Online Access:	Get full text
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