The invention discloses a two-
stroke piston engine air inlet
control system and method based on steering engine angle feedback, and relates to the technical field of
aviation and power machinery. The
system comprises a
CAN bus digital feedback steering engine, an
electronic control unit (ECU), a
crankshaft position sensor, an oil injection control module and a mechanical
throttle valve structure, and four
throttle valves of the horizontally-opposed four-
cylinder engine are controlled to act synchronously through linkage of the single steering engine. The control method is characterized in that an angle detection unit of the steering engine is used for collecting the rotation angle of an output shaft, the rotation angle is transmitted to an ECU through a
CAN bus, the rotation angle is directly mapped into the opening degree of a
throttle valve through a built-in program or
algorithm of the ECU, and a traditional throttle valve
position sensor (TPS) is omitted; the ECU calculates oil injection parameters by combining the
crankshaft rotating speed and the phase signals, drives the oil
injector to act, and meanwhile adjusts the opening degree of the throttle valve in real time through closed-
loop control. The
system structure can be simplified, the cost is reduced, the whole
control system is more compact, the
signal transmission reliability is improved, the response speed is increased, and the
system is suitable for light aircraft power systems such as small unmanned aerial vehicles.