中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
A transformed proportional-integral-derivative controller for a multi-vectored propeller aerostat with independent actuator magnitude and rate saturations

文献类型:期刊论文

作者Chen L(陈丽)1,2; Deng, Yuxiang2; Gao, Qiyuan2; Liu JG(刘金国)1
刊名SCIENCE PROGRESS
出版日期2020
卷号103期号:3页码:1-15
关键词Actuator magnitude saturation actuator rate saturation multi-vectored propeller airship nested saturated PID controller transformed PID controller
ISSN号0036-8504
产权排序1
英文摘要

The problem of designing a controller for a multi-vectored propeller airship with independent amplitude and rate saturations is addressed. First, a linear Proportional-Integral-Derivative (PID) controller is introduced for position control without considering the input saturations. Then, two design methods are applied to the traditional PID control output to satisfy the independent amplitude and rate constraints: the nested saturated PID controller (N-PID) and the transformed PID controller (T-PID). The bounded magnitudes and rate outputs of the modified controllers are given. Simulation results showed both controllers have good tracking performance while satisfying independent amplitude and rate saturations. However, the transformed PID controller has the advantage of expressing explicitly the relationship of the actuator magnitude and rate saturations with the parameters of the transformed function such that the actuator saturations are suppressed by calculation but not by trial and error.

WOS关键词LINEAR-SYSTEMS ; GLOBAL STABILIZATION ; AMPLITUDE ; DESIGN ; FEEDBACK ; MODEL
资助项目National Science Foundation of China[61733017] ; Foundation of State Key Laboratory of Robotics of China[2018O13] ; Shanghai Pujiang Program[18PJD018]
WOS研究方向Education & Educational Research ; Science & Technology - Other Topics
语种英语
WOS记录号WOS:000576106400001
资助机构National Science Foundation of ChinaNational Natural Science Foundation of China (NSFC) [61733017] ; Foundation of State Key Laboratory of Robotics of China [2018O13] ; Shanghai Pujiang ProgramShanghai Pujiang Program [18PJD018]
源URL[http://ir.sia.cn/handle/173321/27731]  
专题沈阳自动化研究所_空间自动化技术研究室
通讯作者Chen L(陈丽)
作者单位1.State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang, China
2.School of Air Transportation, Shanghai University of Engineering Science, Shanghai, China
推荐引用方式
GB/T 7714
Chen L,Deng, Yuxiang,Gao, Qiyuan,et al. A transformed proportional-integral-derivative controller for a multi-vectored propeller aerostat with independent actuator magnitude and rate saturations[J]. SCIENCE PROGRESS,2020,103(3):1-15.
APA Chen L,Deng, Yuxiang,Gao, Qiyuan,&Liu JG.(2020).A transformed proportional-integral-derivative controller for a multi-vectored propeller aerostat with independent actuator magnitude and rate saturations.SCIENCE PROGRESS,103(3),1-15.
MLA Chen L,et al."A transformed proportional-integral-derivative controller for a multi-vectored propeller aerostat with independent actuator magnitude and rate saturations".SCIENCE PROGRESS 103.3(2020):1-15.

入库方式: OAI收割

来源:沈阳自动化研究所

浏览0
下载0
收藏0
其他版本

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。