航空兵器2025，Vol.32Issue(5)：38-45,8.DOI:10.12132/ISSN.1673-5048.2025.0060
具有终端角约束的预设性能自适应滑模制导律
Adaptive Sliding Mode Guidance Law with Prescribed Performance and Terminal Angle Constraint
摘要
Abstract
To address the interception of maneuvering targets in three-dimensional space with terminal impact an-gle constraints and the issue of initial control input saturation,this paper proposes a prescribed performance-based a-daptive sliding mode guidance law capable of suppressing initial input saturation.Firstly,a three-dimensional relative motion model of the missile-target system is established.Then,an extended state observer is designed to estimate dis-turbances caused by target maneuvers,and a prescribed performance function with exponential convergence is intro-duced to constrain system error evolution.Based on this,a novel guidance law is developed by integrating prescribed performance control with adaptive sliding mode control to ensure that the line-of-sight(LOS)angle error remains within a predefined bound.Furthermore,to suppress initial control input saturation,a saturation constraint function is incor-porated into the guidance law design.Finally,comparative simulations under two target maneuvering scenarios are con-ducted.Results demonstrate that the proposed guidance law maintains the LOS angle error within 0.003° and limits the miss distance to less than 0.6 m,achieving high-precision interception while effectively avoiding initial input saturation.关键词
三维拦截制导律/终端攻击角约束/预设性能控制/扩张状态观测器/自适应滑模控制Key words
three dimensional interception guidance law/terminal impact angle constraint/prescribed perfor-mance control/extended state observer/adaptive sliding mode control分类
武器工业引用本文复制引用
姬雨广,纪毅,王少龙,郑昱,范军芳..具有终端角约束的预设性能自适应滑模制导律[J].航空兵器,2025,32(5):38-45,8.基金项目
国家自然科学基金项目(52402442 （）
52272358) （）
中国科协青年人才托举工程项目(YESS20230098) （YESS20230098）
北京市市属高校科研创新教师团队项目(BPHR20220123) （BPHR20220123）
北京市科协青年人才托举工程(BYESS2023310) （BYESS2023310）
