Resumes
Resumes
Brian Fly Phones & Addresses
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69 Cherryville Hollow Rd, Flemington, NJ 08822
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Clinton, NJ
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4128 Holland Dr, Saint Petersburg, FL 33706 (727) 360-4985
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Madeira Beach, FL
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Seminole, FL
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Dunedin, FL
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Clearwater, FL
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Palm Harbor, FL
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Indian Rocks Beach, FL
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Knoxville, TN
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33 Crestview Dr, Clinton, NJ 08809
Work
Position:
Machine Operators, Assemblers, and Inspectors Occupations
Education
Degree:
Associate degree or higher
Business Records
Name / Title
Company / Classification
Phones & Addresses
Principal
Florida Energy Management LLC
Management Services
Management Services
12717 59 Way N, Clearwater, FL 33760
13785 Walsingham Rd, Largo, FL 33774
13785 Walsingham Rd, Largo, FL 33774
Managing
FKI, LLC
13785 Walsingham Rd, Largo, FL 33774
9410 Seminole Blvd, Largo, FL 33772
9410 Seminole Blvd, Largo, FL 33772
Publications
Us Patents
Integrity Of Differential Gps Corrections In Navigation Devices Using Military Type Gps Receivers
View pageUS Patent:
7940210, May 10, 2011
Filed:
Jun 26, 2008
Appl. No.:
12/147410
Inventors:
Brian E. Fly - Clearwater Beach FL, US
Kenneth S. Morgan - St. Petersburg FL, US
James D. Waid - Bradenton FL, US
Martin P. Ignac - Largo FL, US
Kenneth S. Morgan - St. Petersburg FL, US
James D. Waid - Bradenton FL, US
Martin P. Ignac - Largo FL, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
G01S 19/27
G01S 19/41
G01S 19/41
US Classification:
34235724, 34235744, 34235766, 34053913
Abstract:
A method and apparatus for calculating corrections to a navigation solution based on differential GPS data includes receiving GPS ephemeris from at least three GPS satellites. A PVT solution is resolved from the GPS ephemeris. The PVT solution includes a Circular Error Probable (CEP). Differential GPS data for calculating the corrections to the PVT solution is received. A corrected PVT solution is then based upon the differential GPS data. The corrected PVT solution is compared to an area defined by the CEP. Where the corrected PVT solution is not within the area, the corrected PVT solution is rejected in favor of the PVT solution for determining an accurate navigational solution.
Method And System For Forming An Electronic Assembly Having Inertial Sensors Mounted Thereto
View pageUS Patent:
8100010, Jan 24, 2012
Filed:
Apr 14, 2008
Appl. No.:
12/102508
Inventors:
Brian E. Fly - Clearwater FL, US
Dave Moya - Oldsmar FL, US
Dave Moya - Oldsmar FL, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
G01P 1/02
US Classification:
73493, 73510
Abstract:
Systems and methods for forming an electronic assembly are provided. A first inertial sensor having a first sense axis is attached to a bracket. A second inertial sensor having a second sense axis is attached to the bracket such that the second sense axis is substantially orthogonal to the first sense axis. The bracket is attached to a circuit board having at least one microelectronic device mounted thereto.
Methods And Systems For Estimating Weapon Effectiveness
View pageUS Patent:
20050211083, Sep 29, 2005
Filed:
Mar 29, 2004
Appl. No.:
10/811666
Inventors:
James Waid - Bradenton FL, US
Brian Fly - Clearwater FL, US
Brian Fly - Clearwater FL, US
International Classification:
F41F005/00
US Classification:
089001110
Abstract:
Methods and systems for providing an estimate of effectiveness of a selected weapon against a selected target prior to release of the weapon are described. One described method comprises receiving a position uncertainty for a weapon platform, receiving a position uncertainty for a selected target, and determining an ability of the selected weapon to navigate to the selected target. An estimated effectiveness of the selected weapon is determined utilizing one or more of the weapon platform position uncertainty, the target position uncertainty, the navigation capability of the selected weapon, and a kill radius for the selected weapon.