TYE BRADY

Curriculum vitae

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Summary

Accomplished leader, strategic thinker, and engineering professional with over 25 years of hands-on experience in team leadership, technical management, and system design for advanced instrumentation, autonomous vehicles, and robotic systems.

Mission

To make a positive impact through discovery, innovative engineering, and exemplary leadership for the betterment of family, community, and planet.  I do this by creating an environment of innovation, promoting a culture of kindness, and valuing the goodness, strength, and differences of people.

Position Summary

Draper's GENIE Free-Flight Test

Accomplishments Summary

MassRobotics

MAAVRIC

Innovation at Draper

NASA Morpheus

NASA Osiris-Rex

NASA Flight Opportunities

NASA Project M

NASA ALHAT

ISC

Other

Education

Massachusetts Institute of Technology, Cambridge, MA
Master of Science: Aeronautics and Astronautics Engineering, 1999

Boston University, Boston, MA
Bachelor of Science: Aerospace Engineering, 1990

Experience

Chief technologist, Amazon Robotics

September 2015 – Present, North Reading, MA

Lead advanced technology and research efforts into the future to further establish Amazon Robotics as the preeminent industrial robotics company in the world. Guide strategic vision to deliver tomorrow’s industrial operational value while promoting robotics and the benefits they bring worldwide. Represent the Amazon Robotics brand externally to grow its network and attract the world’s best engineers and thinkers to Amazon Robotics. Shape the development and application of robotic technologies for the benefit of Amazon Robotics, it programs and, most importantly, its customers.

Charles Stark Draper Laboratory, Inc., Cambridge, MA

Distinguished Member of the Technical Staff, 2011-2015

With Draper Laboratory as a founding partner, developed and co-founded MassRobotics establishing a new not-for-profit organization to serve as a world-class platform for robotic innovation. Sought and facilitated key external partnerships to promote growth and realize sizable vision.  Recruited key personnel, developed strategic vision, and both designed and executed detailed operational plans to form a world class robotics community across a range of industry value propositions.

Worked directly with CEO to establish a new commercially faced business unit within Draper to promote and capture advanced robotic sensing and perception methods for use on a variety of programs.  Proposed and won over $5M of external funding to develop technologies and autonomous flight methods for a highly dynamic vehicle across a spectrum of unstructured environments.  Established a new internal laboratory and developed a variety of sensing and highly dynamic vehicle prototypes to advance robotic and sensing perception technology readiness.

Led numerous strategic initiatives focused on innovation process, rapid prototyping, and generation of new ideas across variety of program disciplines.  Reported directly to senior management and interfaced with multiple levels of staff culminating in extensive white paper on effective innovation within the Lab.

Technical Director of GENIE team that developed for NASA a fully embedded closed loop integrated Autonomous Guidance, Navigation and Control (AGNC) hardware/software system to perform multiple closed loop Vertical Takeoff Vertical Landing (VTVL) rocket flights.   Field-tested GENIE system over multiple rocket vehicles, trajectories, and test campaigns with great success and numerous press citations.

Space Systems Engineering Group Leader responsible for engineering staff working a variety of commercial, civil, and military space programs.  Responsibilities included performing performance reviews, developing career objectives, and matching staff to projects.

Principal Member of the Technical Staff, 2007-2011

Technical Director for Autonomous Landing and Hazard Avoidance Technology (ALHAT) program that developed an integrated Autonomous Guidance, Navigation and Control (AGNC) hardware and software system with capability to perform global lunar landings under a wide variety of lighting conditions.  Responsibilities as an ALHAT primary architect included managing Draper technical staff, overseeing technical matters, writing technical reports, and developing and executing fundamental system trades for NASA.

Senior Member of the Technical Staff, 2000-2007

Technical Director for a $32M Lunar Access program to develop an autonomous precision lunar landing system for NASA Explorations program.  Managed all aspects of engineering with considerable focus on systems engineering and systems process.  Successfully merged program and technical products with $52M NASA Johnson Space Center ALHAT program that directly supports Explorations Lunar Lander Project Office (LLPO).

Technical Director for multiple spacecraft proposals intended for LEO, GEO, and L2 type orbits.  Worked closely with external customers to develop basic ideas into feasible technical concepts suitable for proposal.  Developed and fostered space hardware roadmap suitable for military space and small satellite markets.

Served as Technical Leader and chief architect for a revolutionary integrated MEMS gyro and star camera assembly called the Inertial Stellar Compass (ISC).  Lead author for technical proposal that won Draper a $10M program. Conceptualized, designed, and led ground validation activity for ISC through all phases of flight program.  Chief Architect of mission operations architecture for ISC flight system under NASA ST-6 guidance.  Lead patent author for ISC (United States Patent 7216036).

Served as Technical Leader and a primary author for NASA proposal that awarded Draper Laboratory $3M for CEV related studies.  Managed team of engineers and MIT faculty that produced mission architectures and vehicle design concepts for future manned missions to the Moon and Mars.

Principal Investigator for $500K internal research project that conceptualized a low power, entirely passive, relative navigation system for use in future autonomous rendezvous spacecraft applications.  Led engineering team through various system processes and design reviews to ensure a robust proof of engineering concept.

Spacecraft Solutions, Inc., Southborough, MA

Consultant, 1999-2000

Founded spacecraft consulting company that specialized in spacecraft digital design, spacecraft instrumentation, and board-level electronic design.  Proven expertise and extensive experience with Actel FPGA tools and spacecraft design techniques. Designed and tested key digital functionality for three internationally based Earth stations used for the HETE-II spacecraft. Provided real-time debugging of critical launch and post-launch anomalies associated with spacecraft.

Massachusetts Institute of Technology, Cambridge, MA

Principal Spacecraft Engineer, 1994-1998

HETE (High Energy Transient Explorer) Project Engineer responsible for key engineering detail of this small, low cost, astronomy spacecraft.  Interfaced regularly with responsible subsystem engineer to understand, develop, and test spacecraft.  Extensive debugging of attitude, power, communications, mechanical, computer, ground station, and ground support equipment issues.  Managed system issues to ensure a robust, nearly autonomous, spacecraft. Directly supported HETE environmental tests that included vibration, shock, and thermal-vacuum tests.  Oversaw and extensively participated in HETE launch operations campaign from initial delivery through launch.  Interfaced with launch contractor on a regular basis explaining key engineering detail.  Reported directly to Principal Investigator.

Senior Spacecraft Engineer, 1992-1994

Co-designer of a CCD based flight instrumentation system known as the LB. The LB was utilized as a UV and optical CCD detector instrument onboard HETE, a pathfinder for the Chandra CCD Imaging Spectrometer (ACIS) program, and also used for CCD calibration and data acquisition efforts within the CCD laboratory.  Advised ACIS design team in areas of software, analog, digital, and systems engineering regarding CCD data acquisition issues and LB use.

Spacecraft Engineer, 1990-1992

Developed testing procedures and performed integration of Analog Electronics (AE) onto ASCA spacecraft.  Designed suite of data acquisition hardware and software tools to characterize flight CCD chips.  Calibrated AE with flight CCDs.

Honors

Patents

Publications

STEINER, T., BRADY, T., HOFFMAN, J.,., “Graph-based Terrain Relative Navigation with Optimal Landmark Database Selection”, IEEE Aerospace Conference, Big Sky, Montana, 7 – 14 March 2015

GREENBAUM, A., BRADY, T., DENNEHY, C., “Understanding International GNC Trends”, IEEE Aerospace Conference, Big Sky, Montana, 7 – 14 March 2015.

BRADY, T., PASCHALL, S., STREETMAN, B., “Guiding Rocket Science with Passion, Purpose, and Team”, GNC 2014: 9th International ESA Conference on Guidance, Navigation & Control Systems”, Porto, Portugal, 2 – 6 June 2014.

PASCHALL, S., BRADY, T., STREETMAN, B., “Demonstrating Autonomous Planetary Landing with GENIE”, GNC 2014: 9th International ESA Conference on Guidance, Navigation & Control Systems”, Porto, Portugal, 2 – 6 June 2014.

COHANIM, B., BRADY, T., “Onboard and Self-Contained Landing Site Selection for Planetary Lander/Hoppers”, IEEE Aerospace Conference, Big Sky, Montana, 1 – 8 March 2014.

PASCHALL, S., BRADY, T., “Rocket Validation of the ALHAT Autonomous GNC Flight System”, IEEE Aerospace Conference, Big Sky, Montana, 1 – 8 March 2014.

GREENBAUM, A., BRADY, T., DENNEHY, C., “Finding the Gaps in Space GNC Hardware”, IEEE Aerospace Conference, Big Sky, Montana, 1 – 8 March 2014.

STEINER, T., BRADY, T., “Vision-based Navigation and Hazard Detection for Terrestrial Rocket Approach and Landing”, IEEE Aerospace Conference, Big Sky, Montana, 1 – 8 March 2014.

COHANIM, B., BRADY, T., “Hazard Detection for Small Robotic Landers and Hoppers”, IEEE Aerospace Conference, Big Sky, Montana, 2 – 9 March 2013.

PASCHALL, S., BRADY, T., “Demonstration of a Safe and Precise Planetary Landing System On-board a Terrestrial Rocket”, IEEE Aerospace Conference, Big Sky, Montana, 3 – 10 March 2012.

SMITH, et al., “The Exoplanet Mission to Detect Transiting Exoplanets with a CubeSat Space Telescope”, 25th Annual AIAA/USU Conference on Small Satellites, Logan, Utah, 8 – 11 August 2011.

BRADY, T., BAILEY, E., CRAIN, T., PASCHALL, S., “ALHAT System Validation”, 8th International ESA Conference on Guidance and Navigation Control Systems, Carlsbad, Czech Republic, 5 – 12 June 2011.

BRADY, T., PASCHALL, S., DEMARS, K., CRAIN, T., BISHOP, R., “GENIE Flight Test Results and System Overview”, AAS 34th Rocky Mountain Guidance and Control Conference, Breckenridge, Colorado, 5 – 9 February 2011.

BRADY, T., “Expanding the Spacecraft Application Base with MEMS Gyros”, SPIE Photonics West Conference, San Francisco, California, 22 – 27 January 2011.

BRADY, T., PASCHALL, S., CRAIN, T., “GN&C Development for Future Lunar Landing Missions”, AIAA Guidance, Navigation, and Control Conference, Toronto, Ontario, Canada 2 – 5 August 2010.

BRADY, T., PASCHALL, S., “The Challenge of Safe Lunar Landing”, IEEE Aerospace Conference, Big Sky, Montana, 6 – 13 March 2010.

CRAIN, T., BISHOP, R., BRADY, T., “Shifting the Inertial Navigation Paradigm with MEMS Technology”, AAS 33th Rocky Mountain Guidance and Control Conference, Breckenridge, Colorado, 6 – 10 February 2010.

BRADY, T., PASCHALL, S., ZIMPFER, D., EPP, C., ROBERTSON, E., “Hazard Detection Methods for Lunar Landing”, IEEE Aerospace Conference, Big Sky, Montana, 7 – 14 March 2009.

COHANIM, B., FILL, T., PASCHALL, S., MAJOR, L., BRADY, T., “Approach Phase Delta-V Considerations for Lunar Landing”, IEEE Aerospace Conference, Big Sky, Montana, 7 – 14 March 2009.

MAJOR, L., BRADY, T., PASCHALL, S., “Apollo Looking Forward: Crew Task Challenges”, IEEE Aerospace Conference, Big Sky, Montana, 7 – 14 March 2009.

PASCHALL, S., BRADY, T., FILL, T., SOSTARIC, R., “Lunar Landing Trajectory Design for Onboard Hazard Detection & Avoidance”, AAS 32th Rocky Mountain Guidance and Control Conference, Breckenridge, Colorado, 2 – 6 February 2009.

BRADY, T. “Next Generation Inertial Stellar Compass”, Space Flight Mechanics Conference, Savannah, Georgia, 8 – 12 February 2009.

EPP, C., ROBERTSON, E., BRADY, T., “Autonomous Landing and Hazard Avoidance Technology (ALHAT)”, IEEE Aerospace Conference, Big Sky, Montana, 1 – 8 March 2008.

PASCHALL, S., BRADY, T., COHANIM, B., “A Self Contained Method for Safe and Precise Lunar Landing”, IEEE Aerospace Conference, Big Sky, Montana, 1 – 8 March 2008.

FOREST, L., COHANIM, B., BRADY, T., “Human Interactive Landing Point Redesignation for Lunar Landing”, IEEE Aerospace Conference, Big Sky, Montana, 1 – 8 March 2008.

BRADY, T., SCHWARTZ, J., “ALHAT System Architecture and Operational Concept”, IEEE Aerospace Conference, Big Sky, Montana, 3 – 10 March 2007.

Brady, T., SCHWARTZ, J., TILLIER, C., “System Architecture and Operational Concept for an Autonomous Precision Lunar Landing System”, AAS 30th Rocky Mountain Guidance and Control Conference, Breckenridge, Colorado, 3 – 7 February 2007.

BRADY, T., BUCKLEY. S, LEAMMUKDA, M., “Space Validation of the Inertial Stellar Compass”, 21st Annual AIAA/USU Conference on Small Satellites, Logan, Utah, 12 – 15 August 2007.

BRADY, T., BUCKLEY. S, TILLIER, C., “Ground Validation of the Inertial Stellar Compass”, IEEE Aerospace Conference, Big Sky, Montana, 6 – 13 March 2004.

BRADY, T., et al. “The Inertial Stellar Compass (ISC): A Multifunctional, Low Power, Attitude Determination Technology Breakthrough”, AAS 26th Rocky Mountain Guidance and Control Conference, Breckenridge, Colorado, 5 – 9 February 2003.

BRADY, T., et al. “The Inertial Stellar Compass: A New Direction in Spacecraft Attitude Determination”, 16th Annual AIAA/USU Conference on Small Satellites, Logan, Utah, 12 – 15 August 2002.

Member

America Institute of Aeronautics and Astronautics (Associate Fellow)
Association of Unmanned Vehicle Systems International (Senior Member)