飞控与探测2025，Vol.8Issue(1)：40-46,7.DOI:10.20249/j.cnki.2096-5974.2025.01.005
基于反步法的旋转弹滑模控制器设计
Design of Sliding Mode Controller for Rotating Missile Based on Backstepping Method
亓国栋 1杨昭 2侯冀川 1翟康瑞 1苌永娜1
作者信息
- 1. 北京机电工程研究所·北京·100074
- 2. 陆装驻北京地区航空军代室·北京·100012
- 折叠
摘要
Abstract
A design method for an adaptive sliding mode controller based on the backstepping method is proposed to address the nonlinear issues of aerodynamic coupling and control coupling during the motion of a rotating projectile.The saturation function is used instead of the sign func-tion to weaken the chattering phenomenon,effectively suppressing the influence of aerodynamic parameter perturbations on control quality,enhancing the robustness of the control system,and a-chieving stable control of the rotating projectile.The stability of the control method was verified using the Lyapunov method,and the effectiveness of the designed method was verified through simulation.关键词
旋转弹/非线性/反步法/滑模控制Key words
rotating projectile/nonlinear/backstepping/sliding-mode control分类
武器工业引用本文复制引用
亓国栋,杨昭,侯冀川,翟康瑞,苌永娜..基于反步法的旋转弹滑模控制器设计[J].飞控与探测,2025,8(1):40-46,7.
