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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Main Authors: Zheng, Zewei, Li, Jiazhe, Feroskhan, Mir
其他作者: School of Mechanical and Aerospace Engineering
格式: Article
語言:English
出版: 2024
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在線閱讀:https://hdl.handle.net/10356/176061
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機構: Nanyang Technological University
語言: English