Controlling internal combustion engine involves varying pilot ignition angle efficiency using transition function when changing from first operating state to second operating state

摘要

The method involves controlling at least one engine operating parameter by forming a pilot ignition angle efficiency depending on engine operating parameters and/or external interventions defining the demand value(s) for the operating parameter(s). The pilot ignition angle efficiency is varied using a transition function when changing from a first operating state into a second operating state.