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MKGN&C Flight Controls Engineer III – Lunar Permanence

Job in Seattle, King County, Washington, 98127, USA
Listing for: Blue Origin LLC
Full Time position
Listed on 2026-06-28
Job specializations:
  • Engineering
    Aerospace / Aviation / Avionics, Systems Engineer, Robotics
Salary/Wage Range or Industry Benchmark: 130706 - 182987 USD Yearly USD 130706.00 182987.00 YEAR
Job Description & How to Apply Below
Position: MK2 GN&C Flight Controls Engineer III – Lunar Permanence
Application close date:

Applications will be accepted on an ongoing basis until the requisition is closed.

At Blue Origin, we envision millions of people living and working in space for the benefit of Earth. We’re working to develop reusable, safe, and low-cost space vehicles and systems within a culture of safety, collaboration, and inclusion. Join our team of problem solvers as we add new chapters to the history of spaceflight!

This role is part of the Lunar Permanence business unit, which develops Blue Origin’s Blue Moon landers and related products. To further Blue Origin's mission of millions of people living and working in space for the benefit of Earth, we are building sustainable infrastructure for our transport of crew and cargo from Earth to the lunar surface.

As part of a hardworking team of engineers, you will join our Guidance, Navigation, and Control (GN&C) team with an emphasis in Flight Controls . You will share in the team’s impact on all aspects of the development of control laws and flight software for spacecraft from Earth to the Moon! You will also prototype algorithms , conduct trade studies for control architectures, and perform linear stability analyses using classical and modern approaches.

Expect to collaborate closely with other subsystems and spacecraft systems engineers to support the development of subsystem boundaries, interfaces, and technical performance measures. In this capacity, you will be responsible for exemplifying best practices, balanced technical judgment, and superior work ethic.

We are looking for someone to apply their technical expertise , leadership skills, and commitment to quality to positively impact safe human spaceflight. Passion for our mission is required !

Minimum Qualifications Minimum of a B.S. degree in Aerospace, Mechatronic, or Electrical engineering or closely related subject areas

Applied industry experience and/or M.S. or Ph.D. focused on development of spacecraft controls

Proven experience in GN&C algorithm development specifically for flight and attitude control using classical and modern control methods

Knowledgeable in frequency domain analysis techniques

Robust understanding of controller stability derivatives and stability margins with respect to flexible body dynamics, slosh dynamics, and spacecraft dynamics

Demonstrated experience with control law design for aerospace vehicles

Familiarity with development of requirements, interfaces, trades and analyses for aerospace GN&C applications

Understand the relationship between attitude control, vehicle configuration, spacecraft dynamics, actuators, sensors, and automation

Experience in Matlab /Simulink and Model Based Development Experience coding in C/C++Robust understanding of software and data configuration management techniques and tools

Excellent written and verbal communication skills

Ability to earn trust and maintain positive and professional relationships

Must be a U.S. citizen or national, U.S. permanent resident (current Green Card holder), or lawfully admitted into the U.S. as a refugee or granted asylum

Preferred Qualifications M.S. or PhD in Aerospace, Mechatronic, Electrical Engineering or closely related technical subject area Proven experience in development, implementation and testing of GN&C systems for aerospace vehicles

Demonstrated technical experience through the full lifecycle of system development

Proficiency in different control law schemes such as PID, Phase-Plane, H-Infinity, Lead and Lag Compensators, Dynamic Inversion, etc.

Experience designing flight control systems with reaction control systems (RCS), cold or hot gas thrusters, thrust vector control (TVC), or electric propulsion

Deep knowledge of astrodynamics, orbital mechanics, attitude kinematics and dynamics

Experience with spacecraft control system design considerations vital for Rendezvous and Proximity Operations and Docking (RPOD).On-orbit experience providing GN&C support during mission operations

Experience synthesizing and evaluating Monte Carlo simulations, hardware-in-the-loop, and software-in-the-loop testing

Experience with real-time flight software and Simulink/Embedded Coder Hands-on experience with…
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