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音圈电机反射镜系统的高精度自适应滑模有限时间控制与实现OA

High-precision adaptive sliding mode finite-time control and implementation for voice coil motor-driven mirror systems

中文摘要英文摘要

为了提升航空动态光学成像系统的控制精度,本研究针对音圈电机驱动反射镜(Voice Coil Motor-Driven Mirror,VCMM)的高精度控制问题,提出了一种基于自适应滑模有限时间控制的综合控制策略.该系统在存在外部干扰和模型不确定性的条件下,仍能实现精确的指令跟踪.首先,基于VCMM的机电特性建立了一般形式的系统动力学模型.其次,构建了一种非线性比例-积分-微分型滑模面,以提高控制系统收敛速度并抑制稳态误差.在此基础上,基于分层抗干扰思想,设计了与模型参数和误差有关的反馈控制项、滑模切换控制项以及自适应控制项,通过Lyapunov稳定性定理严格证明了闭环系统的有限时间内收敛特性.最后,通过对比实验验证了提出的复合控制策略的有效性.实验结果表明,在幅值为180″、频率为1 Hz的正弦指令下,施加周期性有界突变扰动时,该系统跟踪误差的均方根值和峰峰值分别仅为0.28″和4.04″,显著优于常规滑模控制.该控制算法不仅能够保持良好的跟踪性能,对于干扰的抑制性能更优越.本研究为解决高精度航空光电成像系统中的扰动抑制与跟踪控制问题提供了有效方案.

To enhance the control precision of aerial dynamic optical imaging systems,this study address-es the high-precision control problem of Voice Coil Motor-Driven Mirrors(VCMM)by proposing an inte-grated control strategy based on an adaptive sliding mode finite-time control.This strategy enables precise command tracking under conditions of external disturbances and model uncertainties.First,a generalized form of the system dynamics model was established based on the electromechanical characteristics of the VCMM.Second,a nonlinear proportional-integral-derivative type sliding surface was constructed to im-prove the convergence speed of the control system and suppress steady-state errors.Based on this,follow-ing a hierarchical anti-disturbance framework,feedback control terms related to model parameters and er-rors,sliding mode switching control terms,and adaptive control terms were designed.The finite-time con-vergence characteristics of the closed-loop system were rigorously demonstrated using Lyapunov stability theory.Finally,the effectiveness of the proposed composite control strategy was validated through com-parative experiments.Experimental results showed that under a sinusoidal command with an amplitude of 180 arcseconds and a frequency of 1 Hz,and in the presence of periodic bounded disturbances,the system achieved tracking errors with root mean square and peak-to-peak values of only 0.28 arcseconds and 4.04 arcseconds,respectively,significantly outperforming conventional sliding mode control.The proposed control algorithm not only maintains excellent tracking performance but also demonstrates superior distur-bance suppression capabilities.This study provides an effective solution for addressing disturbance rejec-tion and tracking control in high-precision aerial optoelectronic imaging systems.

王丽娜;谷雅楠;梁怀丹;张崇;石广丰

长春理工大学,机电工程学院,吉林 长春 130022长春理工大学,机电工程学院,吉林 长春 130022长春理工大学,机电工程学院,吉林 长春 130022驻长春地区某单位,吉林 长春 130033长春理工大学,机电工程学院,吉林 长春 130022

信息技术与安全科学

音圈电机反射镜航空动态成像系统滑模控制自适应控制有限时间收敛

voice coil mirror-driven mirroraerial dynamic optical imaging systemssliding mode con-troladaptive controlfinite-time convergence

《光学精密工程》 2026 (2)

245-254,10

吉林省科技发展计划项目(No.20250102230JC)国家自然科学基金项目(No.52375405)

10.37188/OPE.20263402.0245

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