Description
Shield AI is a venture-backed defense-tech company with the mission of protecting service members and civilians with intelligent systems.
As a Staff or Senior Staff Engineer (L4/L5), you will take full technical ownership of flight control actuation system design for a Group 5 UAV fighter aircraft. You will work from first principles to define requirements, resolve actuator and integration trades, and drive qualified flight-control actuation hardware from design through production support.
Responsibilities
- System Ownership: Define, allocate, and own the FCAS requirements and verification traceability matrix.
- Actuator Performance: Design and analyze control surface actuation systems, including sizing, dynamic response, bandwidth, redundancy, and failure modes.
- Control-Law Integration: Drive the control law-actuator interface with Flight Controls and Vehicle Management Systems, including actuator dynamics modeling and control surface authority requirements.
- Power and Thermal Integration: Drive actuator power source architecture and load analysis with EPS and hydraulic systems leads, and resolve actuator heat-generation and local thermal-load interfaces with thermal management.
- Structural Integration: Drive coordination of control surface hinge moments and actuator reaction loads with structures.
- Qualification and Hardware Delivery: Define and execute FCAS qualification test plans per MIL-HDBK-516 and MIL-STD-810, using test results to mature qualified flight-control actuation hardware.
- Program Execution: Lead FCAS design-maturity and qualification-status reviews at SRR, PDR, and CDR.
Required qualifications
- Clearance required: US Citizens Only & Must have an Active Secret or higher clearance.
- Experience: 8 to 15 years in flight control actuation system design on fixed-wing aircraft.
- Education: B.S. or M.S. in Mechanical Engineering, Aerospace Engineering, or a related technical discipline.
- Hardware and Supplier Execution: Proven track record sourcing COTS/custom aerospace components, driving suppliers to schedule, and assembling benchtop or vehicle-level test setups.
- Autonomy: Demonstrated ability to self-direct, prioritize technical tasks without oversight, and deliver functional hardware under tight timelines.
- Dynamic Performance: Demonstrated experience with actuator dynamic performance analysis, including bandwidth, response, stability margins, failure mode analysis, and redundancy analysis.
- Integration: Experience coordinating with flight controls and VMS engineers on actuator-control law integration.
- Standards and Reviews: Familiarity with MIL-HDBK-516 and MIL-STD-810 as applied to flight control actuation, and experience supporting SRR, PDR, and CDR on a DoD or fighter-class aircraft program.
Preferred qualifications
- Prior fighter or fighter-adjacent program experience, manned or unmanned.
- Unmanned or autonomous flight control experience, including the redundancy philosophy differences from manned aircraft.
- Experience with EMA or EHA control surface actuators.
This listing is enriched and indexed by YubHub. To apply, use the employer's original posting:
https://jobs.lever.co/shieldai/84ea353d-bd9b-4d1a-8e9c-3b4f31135a2f