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Form of workDraper is an independent, nonprofit research and development company headquartered in Cambridge, MA. The 2,000+ employees of Draper tackle important national challenges with a promise of delivering successful and usable solutions. From military defense and space exploration to biomedical engineering, lives often depend on the solutions we provide. Our multidisciplinary teams of engineers and scientists work in a collaborative environment that inspires the cross-fertilization of ideas necessary for true innovation. For more information about Draper, visit www.draper.com.
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Draper is committed to creating a diverse environment and is proud to be an affirmative action and equal opportunity employer. We understand the value of diversity and its impact on a high-performance culture. All qualified applicants will receive consideration for employment without regard to race, color, religion, sex, disability, age, sexual orientation, gender identity, national origin, veteran status, or genetic information.
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This position will be located at the Draper campus at NASA’s Johnson Space Center (JSC) near Houston, TX. The applicant will join a team of highly motivated Guidance, Navigation and Control (GNC) Engineers in the design, development, test, implementation and operation of spacecraft GNC systems for Earth, Moon, and Mars Missions. We seek applicants who will fit well in this dynamic team while designing challenging GNC systems and developing GNC technologies crucial to Human Exploration missions with our JSC Customer - as well as with customers who value a presence at JSC.
The applicant will be technically involved in various stages in the life cycle of the project including:
- Mission design & architecture trades
- System design & requirement analyses
- GNC algorithms and software development
- GNC system integration & test
The applicant should have strong domain experience in one or more of the following technical disciplines:
- Guidance and Targeting
- Navigation
- Spacecraft Attitude Dynamics and Control Systems
With specialties in one or more of the following:
- Linear covariance analysis
- Rendezvous and prox-ops design and analysis
- Absolute and relative navigation using a variety of sensors
- Sensor characterization and performance analysis
- Entry, Descent and Landing (EDL) systems
- Flight control stability and robustness analysis
- Controls design for a variety of space vehicle systems
Qualifications should include:
- MS degree or higher in a relevant technical field of study.
- Familiarity with several of the following languages and tools: C/C++, Java, and MATLAB, and/or Simulink.
- Experience with FSW development and test – preferably in graphical development environments.
- 6-DOF spacecraft dynamics modeling and simulation.
Security Requirement:
- Applicants selected for this position will be required to obtain and maintain a government security clearance.
