GNC Orbit Controls Engineer
- Compensation
- $130K–$175K / yr
- Location
- Burlingame, California
- Work setup
- Onsite
- Seniority
- Not specified
- Employment
- Full time
- Experience
- Not specified
- Category
- Industrial engineering
- Posted
Skills
Must have
- You are familiar with orbital mechanics and simulation and have had exposure with onboard propagators with perturbation models and integrators on flight targets
- You have GNC software experience in C++ and MATLAB for analysis, modeling, and test-vector generation
- You have supported real maneuvers and can reconcile plan versus truth with post-burn estimation
- You are comfortable at the ADCS and propulsion interface for burn pointing and momentum management
Nice to have
- B.S. or M.S. in Aerospace Engineering, Control Systems, Applied Physics, or a related field
- Familiar with electric propulsion including thrust modeling and calibration, long-burn guidance, duty-cycle planning, and thermal constraints
- Experience with orbit propagation algorithms
- Trajectory design and optimization expertise
- Familiarity with CCSDS ephemeris and attitude formats
Full description
Xona is the navigational intelligence company bringing real-time, centimeter-level certainty to any device, anywhere on Earth.
With Pulsar – the world’s most advanced PNT satellite infrastructure in Low Earth Orbit – Xona will offer a future-proof, backwards-compatible global positioning system optimized for absolute precision, superior power, and robust protection.
We're looking for a GNC Orbit Controls Engineer to design and implement the algorithms and onboard software that handle orbit determination, guidance, maneuver execution, and post-maneuver analysis to deliver safe, efficient, and highly automated station-keeping and disposal. We’re building the software that keeps our spacecraft exactly where they need to be.
What You’ll Do
- Develop open-loop and closed-loop controllers for altitude management, station-keeping, and end-of-life disposal
- Implement and maintain onboard orbit propagators, select and validate integrators, and ensure numerical consistency with ground truth
- Build orbit determination pipelines using EKF with GNSS
- Design burns and long-arc trajectories, and optimize delta V and timelines under comm visibility, power and thermal, and operations constraints
- Coordinate burn pointing and wheel momentum strategy with ADCS
- Maintain numerically consistent MATLAB and C++ simulators, create Monte Carlo campaigns, run SIL and HIL tests, and perform post-maneuver reconstruction
Required Qualifications
- You are familiar with orbital mechanics and simulation and have had exposure with onboard propagators with perturbation models and integrators on flight targets
- You have GNC software experience in C++ and MATLAB for analysis, modeling, and test-vector generation
- You have supported real maneuvers and can reconcile plan versus truth with post-burn estimation
- You are comfortable at the ADCS and propulsion interface for burn pointing and momentum management
Desired Qualifications
- B.S. or M.S. in Aerospace Engineering, Control Systems, Applied Physics, or a related field
- Familiar with electric propulsion including thrust modeling and calibration, long-burn guidance, duty-cycle planning, and thermal constraints
- Experience with orbit propagation algorithms
- Trajectory design and optimization expertise
- Familiarity with CCSDS ephemeris and attitude formats
For U.S. Roles: To comply with U.S. Government space technology export regulations, applicant must be a U.S. citizen, lawful permanent resident of the United States (i.e. Green Card holder), or other protected individual as defined by 8 U.S.C. 1324b(a)(3).