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
* tsEducational Background: Bachelor's degree in Aerospace Engineering, Mechanical Engineering, Electrical Engineering, or a related field. A Master's degree is preferre
* d.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 system
* s.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 plu
* s.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 Gi
* t.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 desig
* n.Simulation and Testing: Experience with hardware-in-the-loop testing, satellite simulation, and ADCS algorithm validation. Ability to design and execute comprehensive test plan
s.