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Pike Aerospace Research Corporation


"electronic fuel injection for experimental aviation & off-road"
» STINGRAY III  

Open Source Fuel Injection and Engine Management

Stingray III ECU 3D CAD

* 32 MHz STR730FZ2T7 ARM7TDMIā„¢ 32-Bit Microcontroller (36 MHz MAX).
* 2 Backup master oscillators for failsafe reliability.
* 24 External analog to digital inputs (16) 10-bit (8) 12-bit.
* (8) Analog inputs (12-bit) can be optionally amplified for O2 sensors and the like.

* 12 Current Sink Outputs (10A max. ea.)

* 1 High speed CAN (Controller Area Network) Interface.
* 2 RS232 Serial Interfaces.
* 2 Fuel Pump / General Purpose current sink outputs w/status LEDs.
* 4 Schmitt trigger TTL level timing inputs.
* 2 High efficiency power supplies for failsafe, cool running, reliable power.
* Automatic failover.
* Failover notification and per supply manual or automatic shutdown.
* 5 volt (2 AMP MAX) output for external TTL sensors and peripherals.
* 2 Onboard thermal sensors provide early warning to potential thermal problems.
* 1 Prototype Area and unused controller pins exposed to user accessible pads.
* 2 User defined Input/Output pins.
* 4 Status LEDs onboard.
* 1 JTAG Debugging/re-programming port.
* Optional cockpit interface backlighted 3.5" touch screen, data logger.
* Less than 10 milliseconds boostrap period (from input power applied to running).
* Always running when power is applied, no lockout mode, no clutch-not-depressed mode, etc.


The project is designed to be open to experimentation, providing a prototyping area, and all source code is open source licensed under the GPL. See the Developers page to get involved.


MINI 2440 Cockpit Interface

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