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: | , , |
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格式: | Article |
語言: | English |
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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 |
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