Principal Engineer Guidance Navigation Control
Summary
Job Description
Description
At Northrop Grumman, our employees have incredible opportunities to work on revolutionary systems that impact people's lives around the world today, and for generations to come. Our pioneering and inventive spirit has enabled us to be at the forefront of many technological advancements in our nation's history - from the first flight across the Atlantic Ocean, to stealth bombers, to landing on the moon. We look for people who have bold new ideas, courage and a pioneering spirit to join forces to invent the future, and have fun along the way. Our culture thrives on intellectual curiosity, cognitive diversity and bringing your whole self to work — and we have an insatiable drive to do what others think is impossible. Our employees are not only part of history, they're making history.Designs, develops, implements, verifies and tests algorithms and software and simulation tools to perform guidance, navigation and control of aircraft, spacecraft, submersibles, surface ships, missiles, launch vehicles and upper stages during powered and coast phases of launch, 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 to achieve a desired position, orientation or orbit in space. Control design and analyses processes consist of the development of the control laws and hardware and software requirements for aircraft, launch vehicles and/or spacecraft.
The candidate GNC Engineer will design, develop, implement, verify, and test high-quality software and simulation toolchains. The candidate will be working on a 6 degree of freedom (6DOF) simulation to design and test missile flight code. The applicant will be working with 6DoF simulation models to evaluate system performance. The candidate should have experience with missile flight dynamics, autopilot and guidance design and implementation into the missile flight code. The candidate should have experience with various trajectory optimization software and tools.
Basic Qualifications:
5 Years with Bachelors in Science; 3 Years with Masters; 1 Year with PhD
US Citizen
Experience working with missile guidance and control algorithms
Experience with missile simulation and flight dynamics
Ability to obtain secret clearance
Preferred Qualifications:
Experience with IR discrimination and tracking
Experience designing, tuning, implementing, and testing guidance algorithms and autopilot parameters for guided missiles and/or interceptors.
Control systems theory and flight dynamics proficiency
Proficiency in creating and maintaining analysis tools in C++, MATLAB and Python
Proficiency in C++ development in a Linux environment
Proficiency in MATLAB and Python toolchains
Existing active and in scope secret clearance upon application
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