System Architecture and Design : Lead the development and evolution of the spacecraft ADCS architecture, including the design and integration of sensors, actuators, reaction wheels, magnetoquers and control algorithms to achieve mission requirements.
Algorithm Development : Design and implement advanced ADCS algorithms to support various pointing modes and attitude control scenarios, ensuring precise control over satellite orientation and stability.
Simulation and Modeling : Perform detailed sensor and actuator characterization, modeling, and simulation to predict system performance and optimize the design. Develop and utilize satellite simulators for system validation.
Hardware Integration : Specify, evaluate, and select ADCS components, including reaction wheels, magnetorquers, star trackers, IMUs, and sun sensors. Integrate these components into the spacecraft, ensuring seamless interaction with other subsystems.
Testing and Validation : Develop and execute hardware‑in‑the‑loop (HIL) tests, ground‑based simulations, and in‑orbit commissioning to validate ADCS performance. Troubleshoot and resolve issues during the integration and testing phases.
On‑Orbit Operations : Support on‑orbit guidance, navigation, and control (GNC) system calibration, commissioning, and operations, including maneuver planning and fault management.
Educational Background : Bachelor's degree in Aerospace Engineering, Mechanical Engineering, Electrical Engineering, or a related field. A Master's degree is preferred.
Industry Experience : Minimum of 2‑5 years of experience in spacecraft attitude determination and control, with hands‑on experience in the development, testing, and operation of ADCS systems.
Technical Expertise : Strong knowledge of ADCS components and systems, including sensors (IMUs, magnetometers, star trackers) and actuators (reaction wheels, magnetorquers). Experience with GNC systems is a significant plus.
Programming Skills : Proficiency in C/C++ for embedded systems development, with experience in Python and MATLAB for simulation and data processing. Familiarity with version control systems such as Git.
System‑Level Understanding : Solid understanding of closed‑loop control systems, orbital mechanics, and spacecraft dynamics. Ability to conduct detailed trade‑off analyses to optimize ADCS design.
Simulation and Testing : Experience with hardware‑in‑the‑loop testing, satellite simulation, and ADCS algorithm validation. Ability to design and execute comprehensive test plans.
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