Battery Systems Development Engineer

Battery Systems

BMS

QUALIFICATIONS:
 

  • Graduated from the departments of Electrical, Electronics, or Communication Engineering at universities,
  • Experienced in analog and microcontroller-based circuit design,
  • Proficient in Battery Management System (BMS) circuit design and analysis,
  • Knowledgeable about battery chemistries, battery pack subcomponents, material selection, and production,
  • Experienced in algorithms used in battery systems (State of Charge, State of Health) and modeling of Li-Ion / Li-Po cells (OTC, TIC, etc.),
  • Minimum two years of practical experience in computer-aided PCB design,
  • Proficient in at least two of the following programs: MATLAB, Simulink, PSIM, and LTSPICE,
  • Familiar with communication protocols such as RS232/422/485, CAN-Bus, SPI, I2C, Ethernet,
  • Preferably skilled in military or civilian standards such as MIL-STD-461, MIL-STD-704, D0-160 (Section 16-18),
  • Preferably experienced in battery packaging methods,
  • Able to adapt to a fast-paced work environment with flexible working hours,
  • Proficient in spoken, written, and comprehension skills in English,
  • Willing to travel,
  • Residing in Istanbul or able to relocate.

 

JOB DESCRIPTION:

  • Conduct material selection and architectural designs for battery systems at the cell, module, and pack levels intended for use in Baykar's Aircraft platforms,
  • Plan and execute test processes for battery systems and components in compliance with standards,
  • Troubleshoot potential faults in battery systems,
  • Realize hardware designs necessary for battery systems,
  • Lead hardware improvement activities in battery systems,
  • Model characteristic behaviors of cells and conduct system development activities in battery systems,
  • Lead the development of algorithms such as State of Charge (SoC) and State of Health (SoH) for battery systems,
  • Execute development activities for charging system designs and charge control algorithms,
  • Analyze data obtained from integration and flight tests in aircraft.