Job offer

Analyse attitude pointing and stability requirements, sensor and actuator performance, and ADCS operational constraints.

Develop satellite attitude dynamics and kinematics models, including environmental disturbances, sensors and actuators for simulation.

Design and implement attitude and angular-rate estimation algorithms using simulated measurements from the available sensors.

Design, tune and compare attitude control algorithms for acquisition, hold and reference tracking, accounting for actuator saturation and constraints.

Verify ADCS algorithms through nominal and disturbed simulations, assess pointing accuracy and transient-response metrics, and document results and interfaces.

Undergraduate

Specific Requirements

Item 01: Academic qualifications and other courses. Proven professional experience (punctuation: 30)

Item 02: Specific programming and simulation merits: experience with MATLAB/Simulink, Python or equivalent languages; mathematical modelling, numerical simulation, data processing and version control (punctuation: 25)

Item 03: Specific ADCS merits: knowledge or experience in attitude dynamics and kinematics, space sensors and actuators, state estimation, and attitude controller design and validation (punctuation: 20)

Item 04: Other relevant merits: technical analysis, documenting results, teamwork, autonomy and willingness to learn simulation and control tools (punctuation: 10)