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作品数:742被引量:917H指数:11
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相关机构:清华大学飞思卡尔半导体(中国)有限公司北京理工大学同济大学更多>>
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Predefined-time controller design for a multiple space transportation robots system based on Lp-Norm-Normalized Sign Function
《Chinese Journal of Aeronautics》2025年第2期432-444,共13页Ran TAO Yibo DING Hanyu LI Xiaokui YUE 
co-supported by the National Natural Science Foundation of China(Nos.12372048,12102343);the Key Program of the National Natural Science Foundation of China(No.U2013206);the China Postdoctoral Science Foundation(No.2023M742835);the Guangdong Basic and Applied Basic Research Foundation,China(No.2023A1515011421).
This paper presents a predefined-time controller for Multiple Space transportation Robots System (MSRS), which can be applied in on-orbit assembly tasks to transport modules to pre-assembly configuration quickly. Firs...
关键词:Multiple space transportation robots system On-orbit assemblyPredefined-time stability criterion Composite Lyapunov function Lp-Norm-Normalized Sign Function Predefined-time controller 
Adaptive feedback control of stability in an axial compressor with circumferential inlet distortion被引量:2
《Chinese Journal of Aeronautics》2023年第5期187-201,共15页Juan DU Yang LIU Jichao LI Wenqiang ZHANG Hongwu ZHANG Chaoqun NIE 
co-supported by the National Natural Science Foundation of China(No.51922098);the National Science and Technology Major Project of China(No.2017-Ⅱ-0004-0017);the Special Fund for the Member of Youth Innovation Promotion Association of CAS(No.2018173).
The adaptive feedback control of stability with circumferential inlet distortion has been experimentally investigated in a low-speed,axial compressor.The flat-baffles with different span heights are used to simulate d...
关键词:Circumferential inlet distortion CROSS-CORRELATION Digital signal processing controller Stability control Tip air injection Tip leakage flow 
Reduced-dimensional MPC controller for direct thrust control被引量:3
《Chinese Journal of Aeronautics》2022年第4期66-81,共16页Shuwei PANG Soheil JAFARI Theoklis NIKOLAIDIS Qiuhong LI 
supported by China Scholarship Council(No.201906830081)。
With the development of the aircraft gas turbine engine, a control system should be able to achieve effective thrust control to gain better operability. The main contribution of this paper is to develop a novel direct...
关键词:Computation time Direct thrust control Gas turbine engine Model predictive control Thrust optimization 
Evaluation of conflict-resolution policies on controller taskload
《Chinese Journal of Aeronautics》2021年第5期315-330,共16页Adan Ernesto VELA William SINGHOSE Karen FEIGH John-Paul CLARKE Eric FERON 
funded by NASA(No.NNX08AY52A);FAA Award(No.07-C-NEGIT);Amendment(Nos.005,010,020);Air Force Contract(No.FA9550-08-1-0375)。
In an effort to maintain safety while satisfying growing air traffic demand,air navigation service providers are considering the inclusion of advisory systems to identify potential conflicts and propose resolution com...
关键词:Air traffic control Air traffic management Conflict detection and resolution Decision-support tools Simulation analysis 
Inverted decoupling and LMI-based controller design for a turboprop engine with actuator dynamics被引量:7
《Chinese Journal of Aeronautics》2020年第6期1774-1787,共14页Huairong CHEN Xi WANG Haonan WANG Nannan GU Meiyin ZHU Shubo YANG 
The main objective of the turboprop engine control system is to ensure propeller absorbed power at a constant propeller speed by controlling fuel flow and blade angle. Since each input variable affects the selected ou...
关键词:Actuator dynamics Inverted decoupling Linear Matrix Inequality(LMI) Static output feedback Turboprop engines 
Design for aircraft engine multi-objective controllers with switching characteristics被引量:3
《Chinese Journal of Aeronautics》2014年第5期1097-1110,共14页Liu Xiaofeng Shi Jing Qi Yiwen Yuan Ye 
supported by the National Natural Science Foundation of China (Grant No. 61104146/F030203);Innovation Plan of Aero Engine Complex System Safety by the Ministry of Education Chang Jiang Scholars of China (Grant No. IRT0905)
The aircraft engine multi-loop control system is described and the switching control theory is introduced to solve the regulating and protecting control problems in this paper. The aircraft engine multi-loop control s...
关键词:Aircraft engine Compensatory controller Min/Max switching Multi-objectives control Smooth switching Switching scheme 
Integration of a 5-axis Spline Interpolation Controller in an Open CNC System被引量:4
《Chinese Journal of Aeronautics》2009年第2期218-224,共7页王永章 刘源 韩振宇 邵忠喜 
Key Development Program of Science and Technology of Heilongjiang Province, China (GB05A501)
A 5-axis controller with curve interpolation function is developed to satisfy high-speed and high-precision computer numerical control (CNC) machining of machine parts with complex shapes in the authors-devised open C...
关键词:numerical control systems sculptured surfaces 5-axis machining motion control curve interpolation 
Development of a PC-based Open Architecture Software-CNC System被引量:9
《Chinese Journal of Aeronautics》2007年第3期272-281,共10页MA Xiong-bo HAN Zhen-yu WANG Yong-zhang FU Hong-ya 
Key Development Program of Science;Technology of Heilongjiang Province, China (GB05A501)
As a key te..hnology in the field of advanced manufacturing, an open architecture controller is studied. In order to develop an open architecture software-CNC system on personal computer (PC) according to open modul...
关键词:open architecture controller PC soflware-CNC behavioral model OMAC machine tool 
Controller Design of DES Petri Nets with Mixed Constraint被引量:7
《Chinese Journal of Aeronautics》2005年第3期283-288,共6页陶泽 谢里阳 梁迪 
NationalHighTechResearchandDevelopmentPlanofChina(2001AA412020)
The problem of constructing a Petri net feedback controller, which enforces the conjunction of a set of linear inequalities on the reachable marking of the place and transition modeled by Petri net, is discussed. A ne...
关键词:automation technique CONTROLLER Petri net reduction Petri net discrete event system(DES) 
The Optimization Method of the Sector Partition Based on Metamorphic Voronoi Polygon被引量:8
《Chinese Journal of Aeronautics》2004年第1期7-12,共6页韩松臣 张明 
Voronoi diagram is founded by using computational geometry based on originaldistribution of the waypoints, and then the elements from Voronoi diagram are metamorphosed by usingthe rule for airsppce partition, and the ...
关键词:aero transportation management sector partition voronoi polygon controller' s workload simulated annealing algorithm 
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