Career records & work history
License Records
Brandon Hagen Suarez
Address:
9242 Regents Rd APT E, La Jolla, CA 92037
Licenses:
License #: A4854397
Category: Airmen
Category: Airmen
Brandon Hagen Suarez, 385252 Balboa Arms Dr UNIT 134, San Diego, CA 92117
Brandon Suarez Phones & Addresses
5252 Balboa Arms Dr UNIT 134, San Diego, CA 92117
La Jolla, CA
Cambridge, MA
Brookline, MA
Boston, MA
Tampa, FL
Mentions for Brandon Hagen Suarez
Resumes & CV records
Resumes
Technical Director
Location:
San Diego, CA
Industry:
Aviation & Aerospace
Work:
General Atomics Aeronautical Systems
Technical Director Massachusetts Institute of Technology (Mit) Sep 2009 - Jun 2011
Graduate Student Aurora Flight Sciences Corporation Jun 2009 - May 2011
Aerospace Engineer Nasa Ames Research Center 2007 - 2007
Academy Honeywell Jun 2006 - Aug 2006
System Engineering Intern
Technical Director Massachusetts Institute of Technology (Mit) Sep 2009 - Jun 2011
Graduate Student Aurora Flight Sciences Corporation Jun 2009 - May 2011
Aerospace Engineer Nasa Ames Research Center 2007 - 2007
Academy Honeywell Jun 2006 - Aug 2006
System Engineering Intern
Education:
University of California, San Diego - Jacobs School of Engineering 2017 - 2018
Massachusetts Institute of Technology 2005 - 2011
Master of Science, Masters, Aerospace Engineering
Massachusetts Institute of Technology 2005 - 2011
Master of Science, Masters, Aerospace Engineering
Skills:
Matlab, Engineering, Solidworks, Product Development
Brandon Suarez
Brandon Suarez
Brandon Suarez
Publications & IP owners
Us Patents
Modular Miniature Unmanned Aircraft With Vectored Thrust Control
US Patent:
2011005, Mar 10, 2011
Filed:
Sep 9, 2009
Appl. No.:
12/556225
Inventors:
Adam Woodworth - Melrose MA, US
Brandon Suarez - Tampa FL, US
Brandon Suarez - Tampa FL, US
Assignee:
Aurora Flight Sciences Corporation - Manassas VA
International Classification:
G05D 1/00
B64C 13/00
B64C 13/00
US Classification:
244175
Abstract:
An aircraft for unmanned aviation is described. The aircraft includes an airframe, a pair of fins attached to a rear portion of the airframe, a pair of dihedral braces attached to a bottom portion of the airframe, a first thrust vectoring module and a second thrust vectoring module, and an electronics module. The electronics module provides commands to the two thrust vectoring modules. The two thrust vectoring modules are configured to provide lateral and longitudinal control to the aircraft by directly controlling a thrust vector for each of the pitch, the roll, and the yaw of the aircraft. The use of directly articulated electrical motors as thrust vectoring modules enables the aircraft to execute tight-radius turns over a wide range of airspeeds.
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