A Generalized Super-Twisting Extended State Observer for Angle-Constrained Terminal Sliding Mode Guidance Law

被引:0
作者
Hu, Zhe [1 ]
Xiao, Liang [2 ]
Yi, Wenjun [1 ]
机构
[1] Nanjing Univ Sci & Technol, Natl Key Lab Transient Phys, Nanjing 210094, Peoples R China
[2] Nanjing Univ Sci & Technol, Sch Comp Sci & Engn, Nanjing 210094, Peoples R China
基金
中国国家自然科学基金;
关键词
terminal angle constraint; Lyapunov; guidance law; three-dimensional; time base generator; MANEUVERING TARGETS; PROPORTIONAL NAVIGATION; IMPACT; SYSTEMS;
D O I
10.3390/aerospace12030252
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this article, a novel finite-time convergent three-dimensional terminal sliding mode guidance law is proposed for intercepting maneuvering targets in three-dimensional space with terminal angle constraints. The proposed guidance law introduces a novel generalized super-twisting extended state observer (GSTESO) to estimate the maneuvering target's acceleration and lumped disturbances, enabling quicker convergence to the true values and offering better noise tolerance. Moreover, a time-varying function called time base generator (TBG) is introduced in the design of the sliding surface, forming a new terminal sliding mode function that ensures that the line-of-sight (LOS) angle converges within a small neighborhood of the desired value at interception. It also offers good robustness and higher guidance accuracy, effectively avoiding overload saturation in the initial stages of guidance. Simulation results indicate that the proposed TBG-based finite-time terminal sliding mode (TBGFTTSM) guidance law can reduce overload magnitude and ensure continuous and smooth guidance commands, while the performance of the GSTESO is also validated.
引用
收藏
页数:20
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