Multivariable controller design for a high performance aero-engine

Author(s):  
R. Samar
IEEE Access ◽  
2017 ◽  
Vol 5 ◽  
pp. 27757-27766 ◽  
Author(s):  
Kai Peng ◽  
Ding Fan ◽  
Fan Yang ◽  
Linfeng Gou ◽  
Wei Lv

1922 ◽  
Vol 26 (136) ◽  
pp. 137-148
Author(s):  
A. E. L. Chorlton

The high performance engine, whether military or commercial, is essentially the light one.The motor which made flying possible was an internal combustion engine, and the basic reason of its success was the direct use of an easily volatile fuel of high heat value, namely, petrol.The first engine developed to use this fuel was that of Daimler, and all motor-car, boat and aviation engines have sprung from this engine.In order to more readily have in mind our problem, we can with advantage briefly run through the main aero engines so far constructed with the progressive results of tests.The engine of Gottlieb Daimler is illustrated by Slide No. I. It had automatic inlet valves and exhaust governing, the latter being a point to be noted.The next slide shows the engine of the Wright Brothers. This engine weighed 8.75 lbs. per B.H.P. inclusive; the most successful engine of to-day weighs under 3 lbs. inclusive.


2016 ◽  
Vol 2016 ◽  
pp. 1-8 ◽  
Author(s):  
Xingjian Wang ◽  
Siru Lin ◽  
Shaoping Wang

Attainment of high-performance motion/velocity control objectives for the Direct-Drive Rotary (DDR) torque motor should fully consider practical nonlinearities in controller design, such as dynamic friction. The LuGre model has been widely utilized to describe nonlinear friction behavior; however, parameter identification for the LuGre model remains a challenge. A new dynamic friction parameter identification method for LuGre model is proposed in this study. Static parameters are identified through a series of constant velocity experiments, while dynamic parameters are obtained through a presliding process. Novel evolutionary algorithm (NEA) is utilized to increase identification accuracy. Experimental results gathered from the identification experiments conducted in the study for a practical DDR torque motor control system validate the effectiveness of the proposed method.


2009 ◽  
Vol 2009 ◽  
pp. 1-10 ◽  
Author(s):  
M. Santhakumar ◽  
T. Asokan ◽  
T. R. Sreeram

Hydrodynamic parameters play a major role in the dynamics and control of Autonomous Underwater Vehicles (AUVs). The performance of an AUV is dependent on the parameter variations and a proper understanding of these parametric influences is essential for the design, modeling, and control of high-performance AUVs. In this paper, the sensitivity of hydrodynamic parameters on the control of a flatfish type AUV is analyzed using robust design techniques such as Taguchi's design method and statistical analysis tools such as Pareto-ANOVA. Since the pitch angle of an AUV is one of the crucial variables in the control applications, the sensitivity analysis of pitch angle variation is studied here. Eight prominent hydrodynamic coefficients are considered in the analysis. The results show that there are two critical hydrodynamic parameters, that is, hydrodynamic force and hydrodynamic pitching moment in the heave direction that influence the performance of a flatfish type AUV. A near-optimal combination of the parameters was identified and the simulation results have shown the effectiveness of the method in reducing the pitch error. These findings are significant for the design modifications as well as controller design of AUVs.


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