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Carl R Dins

from Tempe, AZ
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Connected to:
James A Dins, 68David A Dinsbeer, 48James F Dinscore, 49Sara Dinscore, 42Dan R Dinsdale, 84Eric L Dinsdale, 69Helen J Dinsdale, 96Jared R Dinsdale, 41Jodi L Dinsdale, 55Julie M Dinsdale, 59

Carl Dins Phones & Addresses

  • 1302 Secretariat Dr, Tempe, AZ 85284 (480) 831-0082
  • Campbellsport, WI
  • Mesa, AZ

Work

Company: Honeywell Position: Chief engineer

Education

Degree: Bachelor's degree or higher

Skills

Systems Engineering • Aerospace • Engineering Management • Six Sigma • Engineering • Embedded Systems • Electronics • Manufacturing Engineering • Electrical Engineering • Design For Manufacturing • Manufacturing • Fmea

Emails

j***[email protected]

Industries

Aviation & Aerospace

Resumes

Resumes

Carl Dins Photo 1

Chief Engineer

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Location:
Phoenix, AZ
Industry:
Aviation & Aerospace
Work:
Honeywell
Chief Engineer
Skills:
Systems Engineering
Aerospace
Engineering Management
Six Sigma
Engineering
Embedded Systems
Electronics
Manufacturing Engineering
Electrical Engineering
Design For Manufacturing
Manufacturing
Fmea

Publications

Us Patents

Computer Vision Systems And Methods For Aiding Landing Decision

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US Patent:
20220234752, Jul 28, 2022
Filed:
Jan 22, 2021
Appl. No.:
17/155983
Inventors:
- Charlotte NC, US
Gang He - Morristown NJ, US
Min Wu - Beijing, CN
Carl Dins - Tempe AZ, US
Assignee:
HONEYWELL INTERNATIONAL INC. - Charlotte NC
International Classification:
B64D 43/00
H04L 29/08
G06K 9/20
G06K 9/00
G06T 7/73
B64D 45/00
B64D 45/08
G05D 1/10
Abstract:
The present disclosure provides computer vision systems and methods for an aircraft. The computer vision systems and methods identify a runway based on video frame data from a camera mounted to the aircraft, extract runway pixel positions associated with the runway, determine the aircraft position in a real world coordinate frame based on the pixel positions, the aircraft position including an aircraft lateral position and an aircraft elevation, receive predefined aircraft position data and go-around rules for a compliant approach to the runway, calculate an aircraft position deviation based on the aircraft position and the predefined aircraft position data, determine whether the aircraft position deviation is in conformance with the go-around rules, and output an indication of conformity with the go-around rules.

System And Method For Localization Of Safe Zones In Dense Depth And Landing Quality Heatmaps

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US Patent:
20230081722, Mar 16, 2023
Filed:
Sep 14, 2021
Appl. No.:
17/475055
Inventors:
- Charlotte NC, US
Carl A. Dins - Tempe AZ, US
Naman Rawal - Bengaluru Ka, IN
Assignee:
Honeywell International Inc. - Charlotte NC
International Classification:
B64C 39/02
G06K 9/00
G06K 9/62
G06K 9/20
G06T 7/50
G06N 3/02
Abstract:
A system for localization of a safe landing zone comprises at least one image-capture device onboard an aerial vehicle, and an onboard processor coupled to the image-capture device. The processor is operative to execute instructions to perform a method that comprises: receive, from the image-capture device, two or more overlapping images of a landscape underneath the aerial vehicle; generate, based on the overlapping images, a landing zone heatmap of the landscape; identify, based on the landing zone heatmap, one or more regions of the landscape having potential landing zones and obstacles; and determine a location of a safe landing zone using a distance transform of the one or more regions of the landscape. The location of the safe landing zone is in an area within one of the potential landing zones that is farthest from the obstacles. The location of the safe landing zone is then stored in a database.
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Carl R Dins from Tempe, AZ Get Report