Master's degree in Aerospace Engineering, Electrical Engineering, Mechanical Engineering, Physics, or a closely related field, with 1 (one) year of relevant experience in spacecraft, space systems, or precision aerospace systems; equivalent industry or flight-program experience considered. Demonstrated experience designing, integrating, and testing complex spaceflight or high-reliability aerospace systems, with system-level responsibility across multiple subsystems.
Strong background in attitude determination and control systems (ADCS), including inertial sensors, star trackers, reaction wheels, magnetorquers, actuators, estimation and control algorithms, and precision pointing or formation-flying applications. Experience with optical or laser-based systems, such as laser communications, optical terminals, precision pointing mechanisms, optical sensors, or free-space optical testbeds. Experience with circuit board bring-up, debugging, and test; familiarity with mixed-signal electronics, power systems, and low-level hardware/software interfaces. Software experience across multiple environments (e.g., Python, C/C++, embedded systems, Linux), with proficiency in flight software, embedded control, simulation, or hardware-in-the-loop testing.
Experience with laboratory instrumentation, including sensor calibration, optical alignment, signal conditioning, data acquisition, and system-level diagnostics. Experience developing and maintaining engineering documentation, including requirements, interface control documents, test plans, and verification reports. Ability to work effectively in a collaborative academic research environment, mentoring undergraduate and graduate students while coordinating with faculty and external partners.