Controller-Observer Implementation for Cycle-by-Cycle Control of an HCCI Engine

Author(s):  
Nikhil Ravi ◽  
Matthew J. Roelle ◽  
J. Christian Gerdes

This paper presents experimental cycle-by-cycle control of a single cylinder HCCI engine. The controller is developed from a discrete-time nonlinear model presented in previous work. The model captures the behavior of a gasoline direct-injection engine with an exhaust-recompression strategy used to achieve HCCI. This model is linearized about an operating point so as to enable the synthesis of linear controllers. The model states are represented by the temperature and oxygen content of the retained exhaust, and so are not measurable in practice. Therefore, an observer is used to estimate the states based on a measured ignition proxy. The state estimates are then used by a reference-input tracking controller to track a desired system trajectory. Experimental results show tracking of the model outputs that is comparable to tracking achieved in simulation. The controller is also seen to reduce the cycle-to-cycle variability of combustion significantly, particularly at later combustion phasing. This stabilizes combustion, lowers the instances of misfires, and enables steady operation at points that are normally unstable.

2012 ◽  
Vol 466-467 ◽  
pp. 1237-1241
Author(s):  
Yan Hua Wang ◽  
Shi Chun Yang ◽  
Yun Qing Li

To achieve transient flow characteristics at exit of nozzle orifice on gasoline direct injection engine, two phase Euler-Euler schemes was used to simulate the internal flow of the swirl nozzle. Different flow characteristics were calculated in the simulation. Different kinds of nozzle configuration were studied. Cavitaion and swirl flow occured in the nozzles. Injection hole configuration matters more than area variation of swirl tangential slot to discharge coefficient of the studied nozzle. Discharge coefficient changes a little along the injection hole length. The area of the swirl tangrntial slot plays an important throttling action in nozzle internal flow. Smaller area of swirl tangential slot generates larger degree cavitation but smaller mean injection velocity. Turbulence kinetic energy changes with the time of cavitation and swirl field occurring and the nozzle configuration. Before the appearance of cavitation, smaller inclination angle of orifice can generate more turbulence kinetic energy. After that moment, turbulence kinetic energy varies with different configuration. Along injection hole length, turbulence kinetic energy obviously varies. These flow characteristics affect primary atomization and will be as input for next spray simulation. They are also applied to design reference for injection nozzle.


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