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Todd M Fanciullo

from Guilford, CT
Age ~47
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Also known as:
Todd Franciullo, Tedd Fanciullo
Connected to:
Josie Fanciulli, 68Brian P Fancy, 66Carl C Fancy, 58Cory S Fancy, 42Jean A Fancy, 76John R Fancy, 53Mahnaz A Fancy, 55Robin L Fancy, 70Donna Fancyboy, 45Danielle S Fand, 48

Todd Fanciullo Phones & Addresses

  • Guilford, CT
  • 44 Orange St, New Haven, CT 06510
  • Tucson, AZ
  • Atlanta, GA
  • Marana, AZ
  • Ithaca, NY
  • Lake Zurich, IL

Work

Company: Vawd science and technology Jun 2013 Address: Tucson, AZ Position: Director of application development

Education

Degree: MS School / High School: Georgia Institute of Technology 1999 to 2000 Specialities: Aerospace Engineering - Dynamic Systems and Control

Skills

Simulations • System Architecture • Systems Engineering • Testing • Engineering Management • Integration • Embedded Software • Software Development • Matlab • Sensors • Aerospace • Embedded Systems • Simulink • C++ • System Integration Testing • Fpga • Earned Value Management • Python • Software Design • Image Processing • C# • C • Flight Test • Entrepreneurship • Multithreading • Biomedical Engineering • 3D Printing • Business Development • Java • Sql • Leadership Development • Monte Carlo Simulation • Spacecraft • Team Leadership • Android Development • 3D Modeling • Circuit Design • Business Planning • Intellectual Property • Proposal Writing • Linux/Unix • Html 5 • Css • Javascript • Emotional Intelligence • System Integrators • Unmanned Vehicles • Opengl Es

Awards

Excellence in engineering leadership awa... • Excellence in engineering and technology... • Principal systems engineer with honors -... • Senior systems engineer ii with honors -... • Senior systems engineer i with honors - ...

Interests

Wood Working • Dirt Biking and Motorcycling • International Travel • Hiking • Playing Drums • Mountain Biking • Health

Industries

Aviation & Aerospace

Resumes

Resumes

Todd Fanciullo Photo 1

Principal Systems Engineer

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Location:
203 Whitfield St, Guilford, CT 06437
Industry:
Aviation & Aerospace
Work:
VAWD Science and Technology - Tucson, AZ since Jun 2013
Director of Application Development
Raytheon - Tucson, Arizona May 2005 - Jun 2013
Principal Systems Engineer
Univeristy of Arizona Medical Center - Tucson, Arizona Mar 2010 - Sep 2012
Southern Arizona Limb Salvage Alliance (SALSA™) Volunteer
Independent Consulting - Tucson, Arizona Area Jun 2006 - Feb 2009
Consultant
Sikorsky Aircraft - Stratford, Connecticut Jan 2001 - May 2005
Flight Controls Engineer
Education:
Georgia Institute of Technology 1999 - 2000
MS, Aerospace Engineering - Dynamic Systems and Control Cornell University 1995 - 1999
BS, Mechanical and Aerospace Engineering
Skills:
Simulations
System Architecture
Systems Engineering
Testing
Engineering Management
Integration
Embedded Software
Software Development
Matlab
Sensors
Aerospace
Embedded Systems
Simulink
C++
System Integration Testing
Fpga
Earned Value Management
Python
Software Design
Image Processing
C#
C
Flight Test
Entrepreneurship
Multithreading
Biomedical Engineering
3D Printing
Business Development
Java
Sql
Leadership Development
Monte Carlo Simulation
Spacecraft
Team Leadership
Android Development
3D Modeling
Circuit Design
Business Planning
Intellectual Property
Proposal Writing
Linux/Unix
Html 5
Css
Javascript
Emotional Intelligence
System Integrators
Unmanned Vehicles
Opengl Es
Interests:
Wood Working
Dirt Biking and Motorcycling
International Travel
Hiking
Playing Drums
Mountain Biking
Health
Awards:
Excellence in Engineering Leadership Award
Raytheon Missile Systems
Quaterly award for outstanding leadership, performance and mentoring.
Excellence in Engineering and Technology
Raytheon
Raytheon’s highest technical award recognizing the AAVT IRAD achievements in developing a low-cost algorithm test platform that leveraged rapid algorithm prototyping capabilities, thereby reducing cost and minimizing down-time enabling to rapid adaptive control algorithm development.
Principal Systems Engineer with Honors
Raytheon Missile Systems
Senior Systems Engineer II with Honors
Raytheon Missile Systems
Senior Systems Engineer I with Honors
Raytheon Missile Systems

Business Records

Name / Title
Company / Classification
Phones & Addresses
Todd Fanciullo
THE HEALING ARBOR, LLC
Business Services at Non-Commercial Site · Nonclassifiable Establishments
9172 N Jessy Ln, Tucson, AZ 85742

Publications

Us Patents

Surface Contact Override Landing Scheme For A Fbw Rotary-Wing Aircraft

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US Patent:
7742846, Jun 22, 2010
Filed:
Jun 2, 2006
Appl. No.:
11/446464
Inventors:
Todd M. Fanciullo - Tucson AZ, US
Paul Morphy - Williamsville NY, US
Lorren Stiles - Palm City FL, US
Alex Faynberg - Cheshire CT, US
Assignee:
Sikorsky Aircraft Corporation - Stratford CT
International Classification:
G05D 1/00
US Classification:
701 4, 701 2, 701 3, 701 8, 701 9, 701 11, 244 11, 244 13, 244 1711, 244 1723, 244175, 340 52, 340945, 340961, 340963, 340970, 342 29, 342 30, 342 34, 342 36
Abstract:
A method of transitioning from a complex response flight state to a ground operation control state. Pilot intent is determined through collective position information to control the transition. An independent cockpit switch activates an emergency surface contact transition function for use with a fly-by-wire (FBW) flight control system. Once the surface contact transition function is active, FBW control laws transition from a fully augmented flight state, through an augmentation deactivation state and into the surface contact state.

Fly By Wire Static Longitudinal Stability Compensator System

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US Patent:
20060253230, Nov 9, 2006
Filed:
May 3, 2005
Appl. No.:
11/120827
Inventors:
Todd Fanciullo - New Haven CT, US
Phillip Gold - Shelton CT, US
International Classification:
G06F 17/00
US Classification:
701003000, 701011000
Abstract:
A static longitudinal stability (SLS) system provides an unobtrusive airspeed hold function that reacts to the pilot control inputs into the flight control system and the measured states of the aircraft to engage and disengage smoothly without any explicit mode selection by the pilot. The SLS engages airspeed hold when the aircraft is close to trimmed, non-accelerating state. This logic allows the pilot to either fly close to a desired airspeed and let SLS engage, or trim the aircraft in an accelerating/decelerating maneuver and just wait for the SLS to capture a speed when longitudinal acceleration is small. The SLS is not dependant on the pilot specifically selecting this mode, but rather engages and disengages in response to flight control system status and how the aircraft is being maneuvered.
Control profile
Todd M Fanciullo from Guilford, CT, age ~47 Get Report