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Lee Mcneil Etnyre

from Woodland Park, CO
Age ~86

Lee Etnyre Phones & Addresses

  • 233 Parkview Dr, Woodland Park, CO 80863 (719) 686-7564
  • 5903 Harris Ave, Kansas City, MO 64152 (816) 505-9465
  • 6914 N Bales Ave #122, Kansas City, MO 64119 (503) 463-8850
  • 7020 N Bales Ave, Kansas City, MO 64119 (816) 453-4652
  • Parkville, MO
  • 1533 Hitchrack Rd #122, Bailey, CO 80421 (503) 463-8850
  • 2346 Woodlawn Ct NE, Salem, OR 97303 (503) 463-8850
  • Keizer, OR
  • 2602 Croton Dr #122, Newaygo, MI 49337 (503) 463-8850
  • 2602 E Croton Dr, Newaygo, MI 49337
  • Plano, TX

Work

Company: Garmin international Aug 2003 to Aug 2015 Position: Senior systems certification engineer

Education

School / High School: Colorado School of Mines 1977

Skills

Colorimetry • Navigation Systems • Matrices • Algorithms • Numerical Linear Algebra • Geodesy • Well Log Interpretation • Avionics Design • Statistical Data Analysis • Nonlinear Optimization

Emails

Industries

Research

Resumes

Resumes

Lee Etnyre Photo 1

Lee Etnyre

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Location:
233 Parkview Dr, Woodland Park, CO 80863
Industry:
Research
Work:
Garmin International Aug 2003 - Aug 2015
Senior Systems Certification Engineer

Upat Sa (Pty) Ltd Mar 2000 - Aug 2003
Senior Systems Engineer

Arco Oil and Gas Company 1990 - 1993
Senior Petrophysicist

Oxy Jan 1981 - 1990
Petrophysicist

Lockheed Burbank 1974 - 1975
Reliability and Maintainability Engineer
Education:
Colorado School of Mines 1977
Colorado School of Mines 1975 - 1976
Masters, Geophysics
Missouri School of Mines and Metallurgy 1960
Missouri University of Science and Technology 1956 - 1960
Bachelors, Bachelor of Science, Physics
Will Rogers High School 1956
Lafayette High School, St. Joseph, Mo 1956
Skills:
Colorimetry
Navigation Systems
Matrices
Algorithms
Numerical Linear Algebra
Geodesy
Well Log Interpretation
Avionics Design
Statistical Data Analysis
Nonlinear Optimization

Publications

Us Patents

Systems And Methods For Correlation In An Air Traffic Control System Of Interrogation-Based Target Positional Data And Gps-Based Intruder Positional Data

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US Patent:
6799114, Sep 28, 2004
Filed:
Oct 22, 2002
Appl. No.:
10/277769
Inventors:
Lee McNeil Etnyre - Keizer OR
Assignee:
Garmin AT, Inc. - Salem OR
International Classification:
G01S 502
US Classification:
701120, 701301, 701200, 342 29, 340945, 244 1 R
Abstract:
An improved system and methods for correlating an interrogation-based air traffic surveillance intruder, such as an Traffic alert and Collision Avoidance System (TCAS) intruder, and a GPS-based air traffic surveillance target, such as an Automatic Dependent Surveillance Broadcast (ADS-B) target to minimize or eliminate the display of two symbols for the same intruder/target on the CDTI of an aircraft. The method comprises the steps of receiving ADS-B data at a processing unit and calculating select component deltas for the ADS-B data versus an entry in a TCAS intruder file. Progressive weights are assigned to the deltas and the progressive weights are summed, resulting in a total confidence score. Total confidence scores of ADS-B target and TCAS intruder pairs are compared to determine correlation between the ADS-B target and the TCAS intruders.

Systems And Methods For Correlation In An Air Traffic Control System Of Interrogation-Based Target Positional Data And Gps-Based Intruder Positional Data

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US Patent:
6967616, Nov 22, 2005
Filed:
Aug 21, 2004
Appl. No.:
10/923433
Inventors:
Lee McNeil Etnyre - Keizer OR, US
Assignee:
Garmin AT, Inc - Salem OR
International Classification:
G01S007/22
G01S007/04
G01S013/00
US Classification:
342182, 342 29, 342 30, 342 36, 342175, 342176, 342195, 701120, 701300, 701301, 340945, 340963, 340970, 340971, 340977
Abstract:
An improved system and methods for correlating an interrogation-based air traffic surveillance intruder, such as an Traffic alert and Collision Avoidance System (TCAS) intruder, and a GPS-based air traffic surveillance target, such as an Automatic Dependent Surveillance Broadcast (ADS-B) target to minimize or eliminate the display of two symbols for the same intruder/target on the CDTI of an aircraft. The method comprises the steps of receiving ADS-B data at a processing unit and calculating select component deltas for the ADS-B data versus an entry in a TCAS intruder file. Progressive weights are assigned to the deltas and the progressive weights are summed, resulting in a total confidence score. Total confidence scores of ADS-B target and TCAS intruder pairs are compared to determine correlation between the ADS-B target and the TCAS intruders.

Differential Gps Landing System

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US Patent:
60674849, May 23, 2000
Filed:
Mar 23, 1998
Appl. No.:
9/046483
Inventors:
Stephen Vance Rowson - Parkville MO
Craig A. Stull - Kansas City MO
Albert John Van Dierendonck - Los Altos CA
Lee Etnyre - Parkville MO
Glenn Raymond Courtney - Kansas City MO
Assignee:
Airsys ATM, Inc. - Shawnee KS
International Classification:
G06F 1900
US Classification:
701 16
Abstract:
A differential GPS landing system having at least three GPS receivers at known locations in spatial proximity to each other, wherein each GPS receiver independently receives GPS signals from the plurality of GPS satellites and at least three reference stations, wherein each reference station receives a signal from a different two of the at least three GPS receivers and calculates two separate differential corrections for each satellite, wherein each differential correction is independently calculated using the signals received from a different one of the two GPS receivers. The reference stations preferably average the two calculated differential corrections for each satellite to produce an averaged differential correction for each satellite. The system then validates the averaged differential correction for each satellite calculated by each reference station using two integrity monitors, wherein each integrity monitor receives the averaged differential corrections from a different two of the at least three reference stations, and each integrity monitor compares, with respect to each GPS satellite, the averaged differential corrections from the two of the at least three reference stations to produce a validated set of differential corrections, and broadcasts the averaged differential correction for each satellite calculated by one of the three reference stations. The preferred differential GPS landing system further includes a method that utilizes current differential correction error statistics, prior differential correction error statistics and a Bayesian interval estimation bounding process to provide an error bound on the broadcast differential corrections.
Lee Mcneil Etnyre from Woodland Park, CO, age ~86 Get Report