This role involves designing and optimizing the architecture, algorithms, and integration of sensors and actuators to maintain precise satellite orientation.

Responsibilitie

• sSystem 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

**.

Fundamental Requiremen**

• d: Bachelor's degree in Aerospace Engineering, Mechanical Engineering, Electrical Engineering, or a related field. A Master's degree is preferre

s.