ACTUATOR_SATURATION

作品数：65被引量：146H指数：5
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相关机构：南京航空航天大学更多>>
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相关基金：国家自然科学基金中国博士后科学基金国家教育部博士点基金国家重点基础研究发展计划更多>>
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Distributed fixed-time attitude coordinated control for multiple spacecraft with actuator saturation被引量：4
《Chinese Journal of Aeronautics》2022年第4期292-302,共11页Han GAO Yuanqing XIA Xiaopu ZHANG Guangchen ZHANG 
supported by the National Natural Science Foundation of China(Nos.61720106010,62003041);Science and Technology on Space Intelligent Control Laboratory,China(No.KGJZDSYS-2018-05);General Project of Ningxia Natural Science Fund,China(No.2020AAC03234)。
This paper investigates the distributed fixed-time attitude coordinated control problem for multiple spacecraft subject to actuator saturation under the directed topology. First, a distributed fixed-time observer is p...
关键词：Multiple spacecraft Distributed attitude control Fixed-time observer Fixed-time controller Actuator saturation 
LPV modeling and controller design for body freedom flutter suppression subject to actuator saturation被引量：1
《Chinese Journal of Aeronautics》2020年第10期2679-2693,共15页Wei TANG Yu WANG Jiawei GU Zhiwei SUN 
the National Natural Science Foundation of China(No.61573289);Space Science and Technology Fund,and Natural Science Basic Research Plan in Shaanxi Province of China(No.2019JM042);Fundamental Research Funds for the Central Universities of China(No.3102019ZDHKY11)。
In recent years,the Active Flutter Suppression(AFS)employing Linear ParameterVarying(LPV)framework has become a hot spot in the research field.Nevertheless,the flutter suppression technique is facing two severe challe...
关键词：Anti-windup compensation Flutter suppression Linear parameter-varying interpolation Model order reduction SATURATION 
Robust adaptive fault-tolerant control of a tandem coaxial ducted fan aircraft with actuator saturation被引量：15
《Chinese Journal of Aeronautics》2018年第6期1298-1310,共13页Xiaoliang WANG Changle XIANG Homayoun NAJJARAN Bin XU 
This paper is concerned with the robust adaptive fault-tolerant control of a tandem coaxial ducted fan aircraft under system uncertainty, mismatched disturbance, and actuator saturation.For the proposed aircraft, comp...
关键词：Comprehensive controllability Ducted fan aircraft Fault-tolerant Input saturation Robust adaptive control 
Robust attitude coordinated control for spacecraft formation with communication delays被引量：9
《Chinese Journal of Aeronautics》2017年第3期1071-1085,共15页Jian ZHANG Qinglei HU Danwei WANG Wenbo XIE 
co-supported by the National Natural Science Foundation of China(Nos.61633003 and 61522301);Heilongjiang Province Science Foundation for Youths(Nos.QC2012C024 and QC2015064);the Research Fund for Doctoral Program of Higher Education of China(No.20132302110028)
In this paper,attitude coordinated tracking control algorithms for multiple spacecraft formation are investigated with consideration of parametric uncertainties,external disturbances,communication delays and actuator ...
关键词：Actuator saturation Attitude control Communication delays Neural networks Spacecraft formation 
Robust fault-tolerant control for wing flutter under actuator failure被引量：4
《Chinese Journal of Aeronautics》2016年第4期1007-1017,共11页Gao Mingzhou Cai Guoping 
supported by the National Natural Science Foundation of China (Nos. 11132001, 11272202 and 11472171);the Key Scientific Project of Shanghai Municipal Education Commission (No. 14ZZ021);the Natural Science Foundation of Shanghai (No. 14ZR1421000)
Many control laws, such as optimal controller and classical controller, have seen their applications to suppressing the aeroelastic vibrations of the aeroelastic system. However, those control laws may not work effect...
关键词：Actuator fault Actuator saturation Aeroservoelasticity Fault-tolerant control FLUTTER OBSERVER 
Near minimum-time feedback attitude control with multiple saturation constraints for agile satellites被引量：2
《Chinese Journal of Aeronautics》2016年第3期722-737,共16页Liu Xiangdong Xin Xing Li Zhen Chen Zhen Sheng Yongzhi 
supported by the National Natural Science Foundation of China(Nos.51407011,11372034 and 51207145)
Agile satellites are of importance in modern aerospace applications, but high mobility of the satellites may cause them vulnerable to saturation during attitude maneuvers due to limited rating of actuators, This paper...
关键词：Actuator saturation Attitude control Identification Momentum transfer SATELLITES 
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