Software Engineer for Attitude & Orbit Control System Subsytem

Vakansiyanın detalları

Develop and design the Attitude and Orbit Control System for spacecraft, ensuring accurate control and stabilization.
Define the subsystem architecture, considering mission requirements, constraints, and spacecraft specifications.
Coordinate with the structures and mechanisms specialist to place and mount sensors and actuators with unique requirements, like unoccluded field of views or close placement to the center of mass.
Create and implement control algorithms for precise spacecraft attitude determination and orbit control.
Conduct simulations and analyses to validate the performance of the control algorithms.
Collaborate with the broader spacecraft engineering team to integrate AOCS hardware and software components seamlessly.
Conduct testing and verification activities to ensure the functionality and reliability of the AOCS subsystem.
Develop strategies for fault tolerance within the AOCS subsystem to ensure mission continuity in the event of anomalies.
Prepare comprehensive documentation, including subsystem specifications, design documents, and test plans.
Collaborate with cross-functional teams, including systems engineering, propulsion, and mission operations, to ensure seamless integration of the AOCS subsystem.
Communicate effectively with team members and management to convey progress, challenges, and solutions.

Bachelor's or higher degree in Computer Science, Aerospace Engineering, Electrical Engineering, or a related field.
Strong programming skills, preferably in languages such as C, C++, or Python.
Experience with simulation tools such as MATLAB/Simulink.
Strong mathematical background, especially in Linear Algebra and Calculus.
Proficiency in simulation, and algorithm development.
Excellent problem-solving and analytical skills.
Knowledge of space mission operations and spacecraft dynamics.
Proficient in English language, both written and verbal communication.
Familiarity with hardware components, such as reaction wheels, gyroscopes, magnetometer and optic sensors.
Proficiency in control system analysis and experience with control algorithms, including the Kalman Filter and PID.
Familiarity with industry standards and best practices in spacecraft control systems.
Experience in embedded software development for aerospace or real-time systems.