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控制力矩陀螺框架伺服系统期望补偿自适应鲁棒控制
引用本文:王 璐,郭 毓,钟晨星,吴益飞,郭 健.控制力矩陀螺框架伺服系统期望补偿自适应鲁棒控制[J].控制理论与应用,2017,34(9):1143-1150.
作者姓名:王 璐  郭 毓  钟晨星  吴益飞  郭 健
作者单位:南京理工大学 自动化学院,南京理工大学 自动化学院,中国电子科技集团公司第二十九研究所,南京理工大学 自动化学院,南京理工大学 自动化学院
基金项目:国家自然科学基金项目(61773211, 61673214, 61673219), 江苏省重点研发计划项目(BE2015164)资助.
摘    要:本文针对控制力矩陀螺框架伺服系统中存在的参数不确定性、摩擦非线性及外部干扰问题,提出了一种考虑LuGre摩擦的自适应鲁棒控制方法.针对陀螺框架伺服系统未知惯量和阻尼系数、LuGre摩擦参数不确定性及未知外部干扰上界,设计参数更新律对其进行估计.在此基础上,为提高系统对不确定参数及未知干扰的鲁棒性,设计带有期望补偿的自适应鲁棒控制器,可实现对LuGre摩擦非线性的精确补偿,同时减小测量信号噪声及外部干扰对系统的不利影响.应用Lyapunov稳定性理论分析了闭环系统的稳定性.对挠性航天器姿态机动控制的仿真结果,验证了所提方法的有效性.

关 键 词:控制力矩陀螺    伺服系统    自适应控制    摩擦模型    不确定性
收稿时间:2016/11/21 0:00:00
修稿时间:2017/11/8 0:00:00

Desired compensation adaptive robust control for control moment gyroscopes gimbal servo system
WANG Lu,GUO Yu,ZHONG Chen-xing,WU Yi-fei and GUO Jian.Desired compensation adaptive robust control for control moment gyroscopes gimbal servo system[J].Control Theory & Applications,2017,34(9):1143-1150.
Authors:WANG Lu  GUO Yu  ZHONG Chen-xing  WU Yi-fei and GUO Jian
Affiliation:Automation School of NUST,Automation School of NUST,Southwest China Research Institute of Electronic Equipment,Automation School of NUST,Automation School of NUST
Abstract:For the control moment gyroscopes gimbal servo system with parametric uncertainties, friction nonlinearities and external disturbance, an adaptive robust control method considering LuGre friction model is presented. To estimate the unknown inertia and damping coefficient of the gimbal servo system, the LuGre friction parametric uncertainties as well as the unknown upper bound of the external disturbance, a parameter update law is designed. Furthermore, to improve the robustness of the system to parametric variation and external disturbance, a desired compensation adaptive robust controller is designed. It can precisely compensate the LuGre friction nonlinearity and reduce the adverse effect of measurement noise and external disturbance on the system. Stability of the closed-loop control system is proved via Lyapunov technique. The simulation results for a flexible spacecraft attitude maneuver verify the effectiveness of the proposed control law.
Keywords:control moment gyroscopes  servo systems  adaptive control  friction models  uncertainty
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