ECU for UAV Engines
The Moscat ECU (engine control unit) for EFI drone engines is a compact and lightweight unit that provides closed-loop control of fuel injection and ignition, with control algorithms for two-stroke engines as well as options for four-stroke and Wankel rotary engines.
The electronic engine management system also provides a wide range of essential features including propeller pitch control, engine health monitoring, fault diagnosis, engine speed control via throttle-by-wire, and control of a redundant fuel supply.
Specifications:
| Dimensions | 75 x 71 x 20 mm |
| Weight | 80g (including EMI-shielded aluminium enclosure) |
| Power Consumption | < 0.1A @ 12VDC |
| Communications | RS-232 and CAN Bus |
| Analogue Inputs | BARO, MAP, IAT, 2x CHT, 2x EGT, TPS, Fuel Pressure, 2x Hall/VR sensors, BATT, ECU temp |
| Digital Inputs | 2x Engine Speed (hall or VR), Engine Desired Speed (fly-by-wire) |
| Digital Outputs | 2x Fuel Pump (PWM or switch), Throttle Servo, 2x GPIO (e.g. oil pump, pitch actuator, temperature control vanes, heaters) |
