Terminal Angle Constrained Three-Dimensional Disturbance Rejection Guidance via an Incremental Twisting Algorithm

被引:0
|
作者
Hu, Jintao [1 ]
Hu, Qinglei [1 ,3 ,4 ]
Han, Tuo [2 ,3 ,4 ]
机构
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[2] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
[3] Beihang Univ, Hangzhou Int Innovat Inst, Hangzhou 311115, Zhejiang, Peoples R China
[4] Tianmushan Lab, Hangzhou 311115, Peoples R China
基金
中国博士后科学基金; 中国国家自然科学基金; 北京市自然科学基金;
关键词
Incremental guidance; homing guidance; terminal angle constraint; IMPACT;
D O I
10.1109/FASTA61401.2024.10595105
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper proposes an incremental terminal angle constrained guidance law for the interception of maneuvering targets. The guidance commands are first derived based on the nonlinear PD-like twisting control as a base-line. Then, an incremental guidance law of the baseline command is presented based on the incremental twisting algorithm such that the robustness can be further enhanced. The incremental twisting guidance law has a simple structure and exploits the latest guidance information as closed-loop feedback to the system. Numerical simulations are carried out against various maneuvering targets with different terminal angle constraints. Simulation results show that the constructed guidance scheme is effective in achieving desired terminal angles while capturing maneuvering targets.
引用
收藏
页码:1574 / 1578
页数:5
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