Design, analyze, and tune spacecraft attitude and position control loops using time and frequency domain techniques
Design and analyze relative guidance solutions for Rendezvous and Proximity Operations (RPO)
Analyze and test the spacecraft GNC subsystem performance using simulations and other analytic tools
Develop simulation models for sensors and actuators
Document designs, analysis, and test results and create presentation materials

Requirements

Requires an active / current U.S. Government DoD Top-Secret (TS) security clearance at time of application
Bachelor’s degree with 5 years of relevant engineering experience or Master's degree with 3 years or PhD with 1 year of relevant engineering experience
Experience developing software in MATLAB/Simulink and C/C++
Experience in Guidance, Navigation, and Control (GNC) subsystem design, analysis, and testing
Experience with version control tools such as SVN or Git is preferred

Benefits

Health insurance coverage
Life and disability insurance
Savings plan
Company paid holidays
Paid time off (PTO) for vacation and/or personal business

Applicant Tracking System Keywords

Tip: use these terms in your resume and cover letter to boost ATS matches.

Hard Skills & Tools

MATLABSimulinkCC++Guidance Navigation Control (GNC)simulation modelingcontrol loopstime domain techniquesfrequency domain techniquesRendezvous and Proximity Operations (RPO)

Soft Skills

analytical skillsdocumentationpresentation skills

Certifications

U.S. Government DoD Top-Secret (TS) security clearance