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

• المؤلفون الرئيسيون: Zheng, Zewei, Li, Jiazhe, Feroskhan, Mir
• مؤلفون آخرون: School of Mechanical and Aerospace Engineering
• التنسيق: مقال
• اللغة: English
• منشور في: 2024
• الموضوعات: Engineering; Terminal angle constraint; Sliding mode control
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/176061

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,...