AIRCRAFT DIESEL ENGINES CONTROLLED BY FUZZY LOGIC

Abstract

Normally in diesel and gasoline engines, common rail systems are employed. The key factors for correct engine
\npower management are pressure, precision and velocity. Digital computers and PID control systems characterize current
\nsystems. Recovery strategies are used when anomalies occur and engine performance is significantly reduced. So, restoring
\nnormal conditions needs technical assistance. For safety reasons this approach cannot be used in aeronautical, naval and
\nenergy-supply applications. In some cases it is necessary to utilize all the possible energy from the power unit causing
\nsignificant life-reduction of the engine. In this case a progressive reduction strategy should be used and injection law
\nshould be reduced accordingly. For this purpose injection control based on fuzzy logic is more effective. In this case,
\ntraditional PID control systems are substituted by fuzzy logic control. A reference map is introduced in the Full Authority
\nDigital Electronic Control; this map is interpreted by the fuzzy logic control system that adapts the injection law to the
\ncurrent engine situation. This method has been experimented on a common-rail test bed and results are compared with
\ntraditional “binary recovery strategy” FADEC.