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A transformed proportional-integral-derivative controller for a multi-vectored propeller aerostat with independent actuator magnitude and rate saturations
Chen L(陈丽)1,2; Deng, Yuxiang1; Gao, Qiyuan1; Liu JG(刘金国)2
Department空间自动化技术研究室
Source PublicationSCIENCE PROGRESS
ISSN0036-8504
2020
Volume103Issue:3Pages:1-15
Indexed BySCI
WOS IDWOS:000576106400001
Contribution Rank1
Funding OrganizationNational 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]
KeywordActuator magnitude saturation actuator rate saturation multi-vectored propeller airship nested saturated PID controller transformed PID controller
Abstract

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.

Language英语
WOS SubjectEducation, Scientific Disciplines ; Multidisciplinary Sciences
WOS KeywordLINEAR-SYSTEMS ; GLOBAL STABILIZATION ; AMPLITUDE ; DESIGN ; FEEDBACK ; MODEL
WOS Research AreaEducation & Educational Research ; Science & Technology - Other Topics
Funding ProjectNational Science Foundation of China[61733017] ; Foundation of State Key Laboratory of Robotics of China[2018O13] ; Shanghai Pujiang Program[18PJD018]
Citation statistics
Cited Times:1[WOS]   [WOS Record]     [Related Records in WOS]
Document Type期刊论文
Identifierhttp://ir.sia.cn/handle/173321/27731
Collection空间自动化技术研究室
Corresponding AuthorChen L(陈丽)
Affiliation1.School of Air Transportation, Shanghai University of Engineering Science, Shanghai, China
2.State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang, China
Recommended Citation
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.
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