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...
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...
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...
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...
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...
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...
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...
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...
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...
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 ...