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全景式航空相机的离散滑模控制
引用本文:张雪菲,丁亚林,李昕阳,陈志超.全景式航空相机的离散滑模控制[J].控制理论与应用,2012,29(9):1163-1168.
作者姓名:张雪菲  丁亚林  李昕阳  陈志超
作者单位:1. 中国科学院航空光学成像与测量重点实验室;中国科学院长春光学精密机械与物理研究所,吉林长春130033;中国科学院研究生院,北京100039
2. 中国科学院航空光学成像与测量重点实验室;中国科学院长春光学精密机械与物理研究所,吉林长春130033
基金项目:国家“863”高技术研究发展计划资助项目(2009AA7010102).
摘    要:为了提高全景式航空相机镜筒速度控制系统的动态特性,使其具有响应速度快且超调小的特点,本文提出一种基于降维状态观测器的离散滑模控制方法,对镜筒角速度、角加速度进行观测,并对其速度系统进行控制.针对高氏趋近律带来的控制抖振和稳态抖振问题,本文采用幂次函数趋近律的方法,并对这种方法进行了无抖振理论分析以及稳定性证明.最后以某全景式航空相机作为实验平台,将基于幂次函数趋近律的离散滑模控制应用到镜筒速度控制系统中.实验结果表明,本文提出的控制方法能够有效地减小系统的抖振,使镜筒速度控制系统表现出良好的动态品质.

关 键 词:全景式航空相机  降维状态观测器  角速度  角加速度  趋近律  离散滑模控制
收稿时间:2011/10/18 0:00:00
修稿时间:2012/3/16 0:00:00

Discrete-time sliding-mode control in panoramic aerial camera
ZHANG Xue-fei,DING Ya-lin,LI Xin-yang and CHEN Zhi-chao.Discrete-time sliding-mode control in panoramic aerial camera[J].Control Theory & Applications,2012,29(9):1163-1168.
Authors:ZHANG Xue-fei  DING Ya-lin  LI Xin-yang and CHEN Zhi-chao
Affiliation:Key Laboratory of Airborne Optical Imaging and Measurement; Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences; Graduate School, Chinese Academy of Science,Key Laboratory of Airborne Optical Imaging and Measurement; Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences,Key Laboratory of Airborne Optical Imaging and Measurement; Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences; Graduate School, Chinese Academy of Science,Key Laboratory of Airborne Optical Imaging and Measurement; Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences; Graduate School, Chinese Academy of Science
Abstract:A discrete-time sliding-mode control method based on reduced-order state observer is proposed to provide fast response and small overshoot for the drawtube control system of a panoramic aerial camera. In this method, the angular velocity and acceleration of the camera are measured for controlling the velocity system, and a power-function reaching law is proposed to substitute the conventional reaching law for suppressing the control chattering and the steadystate chattering caused by the conventional reaching law. The non-chattering characteristics and the system stability are analyzed theoretically. This controller has been applied to control the drawtube system of a panoramic aerial camera on an experimental platform; the experiment results show that this control scheme can effectively eliminate the chattering and make the drawtube system achieve desired dynamical performances.
Keywords:panoramic aerial camera  reduced-order state observer  angular velocity  angular acceleration  reaching law  discrete-time sliding-mode control
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