In this study, the starting sequence of the commercial micro gas turbine engine was analyzed and the control logic was developed and implemented using Arduino. The starting sequence the engine is composed of five steps: engine cranking, fuel supply, ignition, acceleration, and stabilization. The control logic of the starting sequence is to get the engine to reach a target(Idle) RPM by controlling the sub-components of the engine such as the start motor, fuel pump, glow plug, start valve, and the main valve. And these sub-components are controlled based on measured values of RPM and EGT(Exhaust Gas Temperature) at the start region. The start sequence of the micro turbine engine was analyzed by conducting a set of experiments using a commercial engine, Jetcat P300-RX and its ECU (Jettronics V10). Then the control logic was developed using Arduino and Arduino MEGA-based ECU was implemented onto the micro turbine engine system. MOSFET modules and motor drivers were used to control the sub-components and Hall sensor and K-type thermocouple were applied to RPM and EGT measurements, respectively. Effects of three parameters, fuel flow rate at ignition step, start motor acceleration rate, and fuel flow rate at acceleration step on engine behavior was investigated and optimal values for those parameters were obtained and applied to the control logic. The results showed that a successful starting sequence is achieved with a maximum EGT of less than 700℃ and a start time within 60 seconds using the developed control logic, which is quite similar to the commercial micro turbine behavior.