Model-Based Design on the Application of Active Flow Control System

2014 ◽  
Vol 668-669 ◽  
pp. 478-481
Author(s):  
Liu Wu Shi ◽  
Nai Ming Wu

Active flow control has produced a great many values in the S-shaped inlets. In this study, the pressure gradient is used to characterize the degree of flow reattachment on the S-shaped inlet and be referred as the pressure recovery parameter[1]. A transfer function is established between an input of frequency of the solenoid valve and an output of the pressure gradient. According to the process of model-based design, one of Simulink model created by Different Control Algorithms which are applied to the established system in the simulation is selected to generate C codes automatically. The generated codes are embedded in the ARM7 processor and the test result of the processor is consistent with simulation.

2000 ◽  
Author(s):  
A. Dean Jacot ◽  
Frederick T. Calkins

2015 ◽  
Vol 7 (1) ◽  
pp. 69-81 ◽  
Author(s):  
W. Machunze ◽  
A. Gessler ◽  
T. Fabel ◽  
P. Horst ◽  
M. Rädel ◽  
...  

2004 ◽  
Vol 2004 (0) ◽  
pp. 5
Author(s):  
Hiro YOSHIDA ◽  
Takehiko SEGAWA ◽  
Hiroyuki ABE ◽  
Yoshihiro KIKUJIMA ◽  
Akira NISHIZAWA

2002 ◽  
Author(s):  
A. Dean Jacot ◽  
Frederick T. Calkins ◽  
Josef Smith

Author(s):  
Karl Neuhäuser ◽  
Rudibert King

Abstract This work is part of a research initiative that aims at increasing the overall gas turbine efficiency by means of constant volume combustion (CVC). For that purpose, flow control in the compressor becomes important, since unsteady combustion effects that may occur in a CVC are very likely to affect stability and efficiency of the compressor negatively due to flow disturbances. Active Flow Control (AFC) often has to deal with uncertain flow conditions, e.g., due to turbulence, varying operating ranges, or simply environmental effects. By that, system parameters such as gain or time constants of the system model also become uncertain, making it difficult for control algorithms to ensure optimality or even stable behavior. Robust control in the sense of ℋ∞ control tackles these problems using an uncertainty description and a nominal model of the system. In this contribution, robust control applied to a linear stator cascade is addressed when only a binary control output from solenoid valves is available. Moreover, a surrogate control variable is proposed, describing the extent of the velocity deficit. By means of a principal component analysis, this control variable is reconstructed from a single measurement input. AFC is realized via trailing edge blowing. In comparison to proportional valves, solenoid valves are cheaper and offer faster switching times with the drawback of a restricted range of the control output to integer or even binary values. Since the ℋ∞ controller, as well as most other control algorithms, results in a real-valued signal u(t) ∈ ℝ, a sum-up rounding strategy is applied to the controller output, forming a binary control output ub (t) ∈ {0, 1}. Although it is impossible for the two outputs to completely match, unless both are integer-valued, there is proof that the difference of real-valued to binary output is bounded in its integral value. The investigations show that a switching frequency of the valves of 100 Hz is sufficient to ensure that the control error via binary control matches its expected equivalent via real-valued control for the presented system.


2001 ◽  
Author(s):  
A. Dean Jacot ◽  
Frederick T. Calkins ◽  
Jim H. Mabe

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