Modular control system for robotized cells and lines

Author(s):  
Gernot Kronreif ◽  
Robert Probst
1997 ◽  
Vol 30 (1) ◽  
pp. 257-261
Author(s):  
Mahbubur Rahman ◽  
Jouko Heikkala

1985 ◽  
Vol 8 (2) ◽  
pp. 109-121 ◽  
Author(s):  
P.M. Barrie ◽  
A. Cunningham ◽  
P. Mass ◽  
D.W. Pritty ◽  
A. Proudfoot

Author(s):  
Michal Gaska ◽  
Grzegorz Kasprowicz ◽  
Adam Flis ◽  
Lech Mankiewicz ◽  
Ewelina Knapska ◽  
...  

2013 ◽  
Vol 850-851 ◽  
pp. 600-603 ◽  
Author(s):  
Yan Liu ◽  
Yong Gang Wang ◽  
Jin Kai Xu ◽  
Xiao Zhou Li

The paper introduces a kind of inspection robot for high-voltage transmission lines from two parts:Mechanical structure and control system. Three arms is adopted in the mechanical structure, while the control system used a hierarchical modular control scheme is designed to a kind of three-layer control structure including the ground monitoring layer, the task decision layer and the action execution layer. The PC/104 and AT89C51 is used for the main control computer, and the MX-servo is used for the power drive components. Except for describing the robots working process of crossing obstacles in detail, the paper also introduces the responsibilities, hardware components, software design process of the control system. From the simulation experiment on motion control system using Matlab/Simulink, we can conclude that the motion control system of the robot has high-stability and reliability and meet the design requirements.


1973 ◽  
Vol 20 (3) ◽  
pp. 552-554 ◽  
Author(s):  
W. H. DeLuca ◽  
A. J. Maier ◽  
J. E. Michelsen ◽  
C. A. Swoboda

2018 ◽  
Vol 2018 ◽  
pp. 1-16 ◽  
Author(s):  
Rudolf Andoga ◽  
Ladislav Főző ◽  
Jozef Judičák ◽  
Róbert Bréda ◽  
Stanislav Szabo ◽  
...  

Improvements in reliability, safety, and operational efficiency of aeroengines can be brought in a cost-effective way using advanced control concepts, thus requiring only software updates of their digital control systems. The article presents a comprehensive approach in modular control system design suitable for small gas turbine engines. The control system is based on the methodology of situational control; this means control of the engine under all operational situations including atypical ones, also integrating a diagnostic system, which is usually a separate module. The resulting concept has been evaluated in real-world laboratory conditions using a unique design of small turbojet engine iSTC-21v as well as a state-of-the-art small turbojet engine TJ-100. Our results show that such advanced control system can bring operational quality of an engine with old turbocompressor core iSTC-21v on par with state-of-the-art engines.


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