Steady‐state dual‐rate Open‐loop transfer function model‐based ripple‐free design

Author(s):  
Ryota Yasui ◽  
Natsuki Kawaguchi ◽  
Takao Sato ◽  
Nozomu Araki ◽  
Yasuo Konishi

Author(s):  
Aimee S. Morgans ◽  
Ann P. Dowling

Model-based control has been successfully implemented on an atmospheric pressure lean premixed combustion rig. The rig incorporated a pressure transducer in the combustor to provide a sensor measurement, with actuation provided by a fuel valve. Controller design was based on experimental measurement of the open loop transfer function. This was achieved using a valve input signal which was the sum of an identification signal and a control signal from an empirical controller to eliminate the non-linear limit cycle. The transfer function was measured for the main instability occurring at a variety of operating conditions, and was found to be fairly similar in all cases. Using Nyquist and H∞-loop shaping techniques, several robust controllers were designed, based on a mathematical approximation to the measured transfer function. These were implemented experimentally on the rig, and were found to stabilise it under a variety of operating conditions, with a greater reduction in the pressure spectrum than had been achieved by the empirical controller.



1997 ◽  
Vol 30 (11) ◽  
pp. 489-494
Author(s):  
Lianming Sun ◽  
Wenjiang Liu ◽  
Akira Sano


2010 ◽  
Vol 173 (1) ◽  
pp. 51-59 ◽  
Author(s):  
Hiroki Ishikawa ◽  
Ryoko Komaki ◽  
Haruo Naitoh ◽  
Akira Yamaba ◽  
Hiroki Katoh


2013 ◽  
Vol 706-708 ◽  
pp. 1038-1041
Author(s):  
Lin Li ◽  
Jun Xu ◽  
Fu Lei Zheng

Based on the analysis of pilot handling behavior characteristics, this paper establishes the pilot transfer function model. According to the characteristics of closed-loop pilot-vehicle system and the relationship between pilot and flight quality, the specific calculation method of pilot model steady state gain was given. Take the aircraft roll angle manipulation for example, and simulate the pilot's manipulation of aircraft of dynamic process. The results show that: the pilot model steady state gain calculation method is simple and feasible, and have a certain reference value for the analysis of closed-loop pilot-vehicle system.





2019 ◽  
Vol 52 (26) ◽  
pp. 88-93
Author(s):  
Alina Voda ◽  
Olivier Martin ◽  
Paulo Rodrigues Naves Neto ◽  
Jean-Dominique Gascuel ◽  
Sebastien Schmerber


2021 ◽  
Vol 2070 (1) ◽  
pp. 012114
Author(s):  
P K Juneja ◽  
S K Sunori ◽  
A Sharma ◽  
A Sharma ◽  
P Kumar ◽  
...  

Abstract In present analysis, response of a selected delayed first order process model is compared for various orders of approximation of dead time present in the transfer function model. Effect of different orders of approximation of dead time is analysed on the open loop step response of the system in terms of percentage change in original and dead time approximated system models. For this purpose, consistency parameter in a headbox of a paper machine is selected as a process model as it closely approximates to a first order delayed process model.



2008 ◽  
Vol 128 (8) ◽  
pp. 1029-1036
Author(s):  
Hiroki Ishikawa ◽  
Ryoko Komaki ◽  
Haruo Naitoh ◽  
Akira Yamaba ◽  
Hiroki Katoh


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