Designs, develops, implements, verifies and tests algorithms to perform guidance, navigation and control of aircraft, spacecraft, launch vehicles and upper stages during powered and coast phases of flight, earth orbit, interplanetary cruise and orbital insertion, as well as during staging events. Navigation functions include the statistical processing of measured data points and their substitution into algorithms simulating physical reality. Guidance functions include the formulation of specific equations and control laws to achieve a desired position in space. Control design and analyses processes consist of the development of the control requirements for aircraft, launch vehicles and/or spacecraft.
About the Role:
We are seeking an experienced Guidance, Navigation, and Control (GNC) Engineer for the Space Based Interceptor (SBI) program. The role will perform technical execution scope associated with missile flight vehicle control system design, guidance and algorithm development, software integration, sensor/actuator system modeling, performance analysis, hardware integrated testing, and flight testing.
- B.S. or M.S. in Aerospace Engineering, Mechanical Engineering, Electrical Engineering, or related field.
- Strong foundation in missile or satellite flight dynamics, stability, and control theory (e.g., classical, state space, optimal, robust, adaptive).
- Proficient in MATLAB/Simulink for modeling, linearization, and/or Monte Carlo analysis.
- Familiarity with high fidelity 6-DoF simulations and experience designing and/or maintaining control system models.
- Knowledge of software methods or standards including safety critical items and/or version control systems (e.g., Git, Gitlab).
- Ability to develop and execute unit, integration, and/or system level tests (e.g., HIL, SIL, flight test).
- Strong written and oral communication skills for cross functional teams and senior leadership.
- Experience with Missile or Satellite Attitude Control System (ACS) or Thrust Vector Control (TVC) hardware/software, regardless of actuation type (e.g., hydraulic, electromechanical, flexible nozzle, RCS, etc.).
- Experience with stability & control analysis and guidance law development.
- Experience modeling GNC interaction with solid propellant systems, including transients, and thrust misalignment.
- Experience in development and integration of a 6-DoF high-fidelity vehicle simulation that includes thrust vector control and bending structural dynamics.
- Demonstrated experience with test and tactical flight algorithm performance evaluation in the frequency and time domains.
- Proven ability to implement and optimize control algorithms within embedded software or firmware applications for ACS or TVC.
- Experience translating control algorithms from MATLAB/Simulink into flight-ready embedded C/C++ software, including auto-code generation.
- Familiar with agile development methodologies and processes.
- Familiar with Hardware-in-the-Loop (HIL) test environments with models that accurately emulate actuator dynamics and sensor noise.
- Experience in planning and execution of hardware tests or flight tests, telemetry handling, and post-test analysis, or reconstruction.
Pay Information
Full-Time Salary Range: $122600.00 - $227600.00
At Lockheed Martin, we know mission success starts with taking care of our people. Our Total Rewards program is designed to attract top talent, support your well-being, and help you grow—both professionally and personally.
The salary range for this position is as listed on the requisition. Please note that the salary information listed is a general guideline only. Lockheed Martin considers factors such as (but not limited to) scope and responsibilities of the position, candidate's work experience, education/ training, key skills as well as market(work location) and business considerations when extending an offer.
Benefits offered: Medical, Dental, Vision, Flexible work arrangements and schedules (e.g., 4x10), 401(k) match, Paid time off, Holidays, Parental Leave, EAP, Flexible Spending Accounts, Education Assistance, Life Insurance, Short-Term Disability, and Long-Term Disability.
- Annual short-term and/or long-term incentive compensation programs may be offered depending on the position. Payments under these annual programs are not guaranteed and can vary from year to year and are tied to a range of performance metrics.
- For (Washington state applicants only) Non-represented full-time employees: accrue at least 10 hours per month of Paid Time Off (PTO) to be used for incidental absences and other reasons; receive at least 90 hours for holidays. Represented full time employees accrue 6.67 hours of Vacation per month; accrue up to 52 hours of sick leave annually; receive at least 96 hours for holidays. PTO, Vacation, sick leave, and holiday hours are prorated based on start date during the calendar year.
Lockheed Martin Aurora, Colorado, USA Office
Aurora, United States
Lockheed Martin Castle Rock, Colorado, USA Office
Castle Rock, United States
Lockheed Martin Denver, Colorado, USA Office
Denver, United States
Lockheed Martin Englewood, Colorado, USA Office
Englewood, United States
Lockheed Martin Lakewood, Colorado, USA Office
Lakewood, United States
Lockheed Martin Littleton, Colorado, USA Office
Littleton, United States
Lockheed Martin Thornton, Colorado, USA Office
Thornton, United States
Similar Jobs
What you need to know about the Colorado Tech Scene
Key Facts About Colorado Tech
- Number of Tech Workers: 260,000; 8.5% of overall workforce (2024 CompTIA survey)
- Major Tech Employers: Lockheed Martin, Century Link, Comcast, BAE Systems, Level 3
- Key Industries: Software, artificial intelligence, aerospace, e-commerce, fintech, healthtech
- Funding Landscape: $4.9 billion in VC funding in 2024 (Pitchbook)
- Notable Investors: Access Venture Partners, Ridgeline Ventures, Techstars, Blackhorn Ventures
- Research Centers and Universities: Colorado School of Mines, University of Colorado Boulder, University of Denver, Colorado State University, Mesa Laboratory, Space Science Institute, National Center for Atmospheric Research, National Renewable Energy Laboratory, Gottlieb Institute
