Support the design, development, integration, verification, and operational support of GNC subsystems for Earth observation and telecommunications satellites.
Responsibilities
Define GNC functional, performance, and safety requirements and maintain requirements traceability
Develop system documentation, including specifications and Interface Control Documents (ICDs)
Perform orbital and attitude dynamics modelling, simulation, and performance analyses
Design and validate attitude determination, orbit determination, and control algorithms
Develop control laws for three-axis stabilization, attitude maneuvers, and station-keeping
Requirements
Bachelor’s degree in Aerospace Engineering, Electrical Engineering, Physics, or a related field