As an Aerospace Guidance Engineer, you will develop, implement, and verify guidance algorithms for real-time trajectory optimization for Human Landing Systems (HLS) project that will take humans back to the Moon.

Trajectory analyses will be based on fundamental principles of orbital mechanics, with increasing levels of fidelity and complexity added as more detailed modeling is required.

Monte Carlo, design of experiments, and other methods will be used to assess vehicle and stage performance.

Trajectories for ascent, descent, rendezvous, proximity operations, and docking will be analyzed in support of trade and sensitivity studies affecting system configuration and mission designs.

Job Requirements:

A degree in Aerospace Engineering, Mechanical Engineering, or related field is required. A degree from an ABET-accredited university is preferred.

(9KQ) Typically, educational requirements are the equivalent of a Ph.D. with a minimum 4 years of experience; MS with at least 8 years of experience, or a BS with at least 10 years of experience.

(9KR) Typically, educational requirements are the equivalent of a Ph.D. with a minimum 19 years of experience; MS with at least 23 years of experience, or a BS with at least 25 years of experience.

Required Skills and Experiences:

Strong evidence of the following skills is needed:

Python, C++, and/or Matlab, Matlab Simulink

Trajectory Optimization

Numerical optimization

Optimal Control