FCAS Systems Engineer for Flight Control System Design (f­­/­­m­­/­­d) für AIRBUS Defence and Space

- Requirements Engineering: Manage requirements throughout the entire flight control system development cycle using the V-Model - Requirements Analysis: Analyse, define, derive and partition requirements across all design levels - Concept Development: Support, write and assess concepts and feasibility studies - System Function Specification: Define and develop FCS general system functions Integration: Ensure seamless integration of the autoflight and primary control law design requirements with general FCS functions - Interface Coordination: Define and coordinate interfaces with other aircraft systems, including writing Interface Control Documents (ICDs) - Assessments: Perform and coordinate system design assessments for the clearances - Software Testing: Define and monitor software acceptance test (SAT) objectives, ensuring comprehensive coverage