Built on the domestic, military-grade RapidECU electronic control platform and targeting aerospace equipment such as electric UAVs, new-energy aircraft and launch-vehicle auxiliary power systems, this solution addresses pain points of high-altitude low pressure, high/low-temperature cycling, strong vibration and shock, efficient energy scheduling and classified-data closed loops. It provides a one-stop new-energy powertrain control unit (PCU) solution spanning rapid prototyping, control algorithm validation, HIL simulation testing and batch fielding, coordinating motor control, battery management, energy distribution, thermal management and fault protection. The entire process complies with aerospace reliability, self-controllability, security and functional-safety requirements, fitting the combat, test and O&M needs of various aerospace new-energy powertrain equipment.

The engine ECU is a key component of the electronic control system of an electronically controlled engine (comprising sensors, actuators and the electronic control unit (ECU)). Its function is to acquire and process input signals from various sensors, perform control-decision calculations according to engine operating requirements (injection pulse width, ignition advance angle, etc.), and output the corresponding control signals. In addition to fuel injection control, today's electronically controlled engines also control ignition, EGR, idling and the wastegate of turbocharged engines. Since a single ECU is used to comprehensively control the engine, it is also called the engine management system.