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Matthew J Carrico

from Mount Vernon, IA
Age ~66
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Also known as:
Matthew John Carrico, Matt J Carrico
Phone and address:
303 Abbe Hills Rd, Mount Vernon, IA 52314
(319) 895-6325
Related to:
Brenda M Marker, 74James D Carrico, 33Polly Carrico, 32Debora Carrico, 65
Connected to:
Bobby L Carrico, 68Dana C Carrico, 36Florence V Carrico, 75Joie D Carrico, 73Lisa M Carrico, 63Walker L Carrico, 26Rondale W Carridine, 52Jasmine M Carrie, 37Jeanne R Carrie, 74Pam Carrie

Matthew Carrico Phones & Addresses

  • 303 Abbe Hills Rd, Mount Vernon, IA 52314 (319) 895-6325
  • Cedar Rapids, IA

Work

Company: Rockwell collins Position: Fellow

Industries

Aviation & Aerospace

Public records

Vehicle Records

Matthew Carrico

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Address:
303 Abbe Hl Rd, Mount Vernon, IA 52314
VIN:
JM1CR2W36A0364909
Make:
MAZDA
Model:
MAZDA5
Year:
2010

Resumes

Resumes

Matthew Carrico Photo 1

Fellow

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Location:
Cedar Rapids, IA
Industry:
Aviation & Aerospace
Work:
Rockwell Collins
Fellow

Publications

Us Patents

Aircraft Traffic Source Selection And Display System And Method

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US Patent:
7148816, Dec 12, 2006
Filed:
Aug 30, 2004
Appl. No.:
10/929250
Inventors:
Matthew J. Carrico - Mount Vernon IA, US
Assignee:
Rockwell Collins, Inc. - Cedar Rapids IA
International Classification:
G08G 5/04
US Classification:
340961, 340971, 701 14
Abstract:
A method of displaying traffic information is disclosed. The method comprises providing traffic information from at least one of a first and a second traffic information system to a traffic display system. The method also comprises choosing to display, by the traffic display system, traffic information from the first traffic information system when no traffic information from the second traffic information system is available. Further, the method comprises choosing to display, by the traffic display system, traffic information from the second traffic information system when no traffic information from the first traffic information system is available. The method further comprises choosing to display, by the traffic display system, traffic information from either the first traffic information system or the second traffic information system using a predetermined selection algorithm when traffic information is available from both traffic information systems. Further still, the method comprises choosing to display, by the traffic display system, traffic information from the first traffic information system when an advisory condition is indicated by the first traffic information system.

Large Error To Desired Path Correction Indicator

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US Patent:
7508322, Mar 24, 2009
Filed:
Mar 3, 2006
Appl. No.:
11/368075
Inventors:
Michael J. Krenz - Cedar Rapids IA, US
Arlen E. Breiholz - Cedar Rapids IA, US
Matthew J. Carrico - Mount Vernon IA, US
Kenneth W. Mc Elreath - Mount Vernon IA, US
Assignee:
Rockwell Collins, Inc. - Cedar Rapids IA
International Classification:
G01C 21/00
US Classification:
340976, 340971, 340979, 340972, 340975, 701302, 701 16
Abstract:
A current path display indicator for a display device of a vehicle. The current path display indicator includes a flight path indicator (FPI) and a visual cue associated with the FPI to indicate relative direction from the vehicle's current path to a desired path. The visual cue may be embodied in possibly a number of different ways. For example, it may be embodied as an arrow extending from a circular portion of the FPI; a highlighted segment superimposed on the circular portion of the FPI; a triangle extending from the circular portion; or, a pie-shaped marker contained within the circular portion.

Detecting And Alerting Before An Aircraft Leaves An Approved Or Safe Region Of Operation

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US Patent:
7668628, Feb 23, 2010
Filed:
Sep 19, 2005
Appl. No.:
11/230246
Inventors:
Matthew J. Carrico - Mount Vernon IA, US
Assignee:
Rockwell Collins, Inc. - Cedar Rapids IA
International Classification:
G01C 23/00
G05D 1/00
US Classification:
701 9, 342 29, 340961, 340963, 701 3, 701 8
Abstract:
Methods and systems are provided which warn a pilot or flight crew to prevent navigation of an aircraft into an unapproved region of operation. A boundary of an approved region of operation for the aircraft is identified. A position of the aircraft relative to the boundary of the approved region of operation is determined. Then, a warning is generated if the determined position of the aircraft relative to the boundary of the approved region of operation satisfies a predetermined criteria.

Runway And Airport Incursion Alerting System And Method

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US Patent:
8019529, Sep 13, 2011
Filed:
Aug 17, 2007
Appl. No.:
11/893728
Inventors:
Vivek Sharma - Kirkland WA, US
Joel M. Wichgers - Urbana IA, US
Matthew J. Carrico - Mount Vernon IA, US
Sethu R. Rathinam - Cedar Rapids IA, US
Stefan Koczo, Jr. - Cedar Rapids IA, US
Assignee:
Rockwell Collins, Inc. - Cedar Rapids IA
International Classification:
G08G 5/06
G06F 19/00
US Classification:
701117, 701301
Abstract:
An apparatus for detecting incursions for an aircraft and surface vehicles includes an incursion processor receiving ownship position from an ownship navigation processor, traffic information from a traffic surveillance processor, and obstacle information from an obstacle detector and generating alert information. The apparatus also includes a display processor receiving airport chart information and providing display information for displaying the alert information and airport chart information.

System, Module, And Method For Presenting Runway Advisory Information To A Pilot

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US Patent:
8193948, Jun 5, 2012
Filed:
Sep 30, 2009
Appl. No.:
12/570019
Inventors:
Geoffrey A. Shapiro - Cedar Rapids IA, US
Alena L. Benson - Seattle WA, US
Matthew J. Carrico - Mount Vernon IA, US
Randy H. Jacobson - Melbourne FL, US
Assignee:
Rockwell Collins, Inc. - Cedar Rapids IA
International Classification:
G08B 23/00
US Classification:
340965, 340969, 340971, 340972, 340980, 340945, 340947, 340951, 340953, 340961, 701 8, 701 9, 701 11, 701 16, 701 18
Abstract:
A present novel and non-trivial system, module, and method for presenting runway advisory information are disclosed. A runway reference may be established using data received from a source of navigation reference data, where such data could represent runway information, runway awareness zone information, landing awareness zone information, and/or runway threshold line information. Navigation data representative of at least aircraft location and input factor data may be received from a source. Phase of flight may be determined using input factor data, and a runway advisory data set may be generated as a function of phase of flight and the positional relationship between aircraft location and the runway reference. Runway advisory data set may be representative of advisory information comprised of visual runway advisory information, aural runway advisory information, tactile advisory information, or a combination thereof. A presentation system receives the runway advisory data set and presents advisory information.

Operational Flight Phase Determination And Indication System

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US Patent:
8217807, Jul 10, 2012
Filed:
Jul 16, 2009
Appl. No.:
12/504524
Inventors:
Matthew J. Carrico - Mount Vernon IA, US
Assignee:
Rockwell Collins, Inc. - Cedar Rapids IA
International Classification:
G01C 21/00
US Classification:
340971, 340945, 340951, 340964
Abstract:
An operational flight phase determination and indication system for an aircraft includes input/output circuitry for receiving an operational flight phase selector output signal and aircraft sensor signals. A processor is coupled to the input/output circuitry. A flight phase data table is coupled to the processor. The flight phase data table includes a list of the defined operational flight phases for the aircraft. A flight phase transition rules set is coupled to the processor. The flight phase transition rules set includes flight rules for defining flight phase transitions. Program memory and working memory are coupled to the processor. The processor uses input from the input/output circuitry, the flight phase data table, the flight phase transition rules set, the program memory and the working memory to provide an operational mode signal indicating the operational mode of the aircraft. A flight phase selector is coupled to the processor for providing the flight phase selector signal to the processor in accordance with the pilot selected flight phase input. A display indicator driver is coupled to the processor for providing display indicator driver signals to an operational flight phase indicator in accordance with the operational mode signal.

Hold Line Awareness Using Tactile Devices

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US Patent:
8386092, Feb 26, 2013
Filed:
Sep 2, 2008
Appl. No.:
12/231388
Inventors:
Matthew J. Carrico - Mount Vernon IA, US
Maureen A. Lehman - Cedar Rapids IA, US
Assignee:
Rockwell Collins, Inc. - Cedar Rapids IA
International Classification:
G06F 17/00
G05D 1/02
G05D 3/12
G08B 21/00
B64C 13/00
US Classification:
701 3, 701 11, 701 45, 701120, 340945, 340965, 340972, 340988
Abstract:
A hold line awareness system for alerting an occupant of an aircraft that the aircraft is approaching a hold line at an airport. In one broad aspect the invention includes an airport database located on an aircraft. The airport database is configured to store location information for a plurality of hold lines at the airport. A positioning system is located on the aircraft. The positioning system is configured to determine the aircraft location. A processor is located on the aircraft and is operatively connected to the airport database and the positioning system. The processor is configured to calculate the distance between the aircraft location and a hold line and provide a processor alerting output signal if the distance is less than a predetermined value. A sensory effector is located on the aircraft and operatively connected to the processor for receiving the processor alerting output signal and providing a tactile alert to an occupant in response thereto. In another broad aspect, a real time feature detecting system is utilized instead of the airport database.

System And Method To Automatically Configure An Aircraft For An Operational Flight Phase

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US Patent:
8493240, Jul 23, 2013
Filed:
Jun 23, 2010
Appl. No.:
12/821335
Inventors:
Matthew J. Carrico - Mount Vernon IA, US
Assignee:
Rockwell Collins, Inc. - Cedar Rapids IA
International Classification:
G01C 21/00
US Classification:
340971, 340945, 340951, 340964
Abstract:
An operational flight phase determination, indication and configuration system for an aircraft includes input/output circuitry for receiving an operational flight phase selector output signal, aircraft sensor signals, and on-board automation system output signals including configuration status information. A processor is coupled to the input/output circuitry. A flight phase data table is coupled to the processor. The flight phase data table includes a list of the defined operational flight phases for the aircraft. A flight phase transition rules set is coupled to the processor. The flight phase transition rules set includes flight rules for defining flight phase transitions. An aircraft system configuration data table is coupled to the processor. The aircraft system configuration data table includes a list of the defined configurations for each operational flight phase and the aircraft system configuration settings for each configuration. Program memory and working memory are coupled to the processor.
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Matthew J Carrico from Mount Vernon, IA, age ~66 Get Report