Melville D. McIntyre

Person

Bellevue, WA, US

People

Patents Grantslast 30 patents

Information Patent Grant
Alternative method to determine the air mass state of an aircraft a...
- Patent number 9,731,814
- Issue date Aug 15, 2017
- The Boeing Company
- Melville Duncan Walter McIntyre
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Alternative method to determine the air mass state of an aircraft a...
- Patent number 8,761,970
- Issue date Jun 24, 2014
- The Boeing Company
- Melville Duncan Walter McIntyre
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Airspeed sensing system for an aircraft
- Patent number 8,527,233
- Issue date Sep 3, 2013
- The Boeing Company
- Melville Duncan Walter McIntyre
- G01 - MEASURING TESTING
Information Patent Grant
Apparatus and method for navigation of an aircraft
- Patent number 6,654,685
- Issue date Nov 25, 2003
- The Boeing Company
- Melville Duncan W. McIntyre
- G05 - CONTROLLING REGULATING
Information Patent Grant
Skipping filter for inertially augmented landing system
- Patent number 6,549,829
- Issue date Apr 15, 2003
- The Boeing Company
- Leonard R. Anderson
- G01 - MEASURING TESTING
Information Patent Grant
Inertially augmented GPS landing system
- Patent number 6,178,363
- Issue date Jan 23, 2001
- The Boeing Company
- Melville D. McIntyre
- G05 - CONTROLLING REGULATING
Information Patent Grant
Airspeed prediction filter
- Patent number 5,689,251
- Issue date Nov 18, 1997
- The Boeing Company
- Andrew W. Houck
- G01 - MEASURING TESTING
Information Patent Grant
Integrated fault-tolerant air data inertial reference system
- Patent number 5,297,052
- Issue date Mar 22, 1994
- The Boeing Company
- Melville D. W. McIntyre
- G01 - MEASURING TESTING
Information Patent Grant
Integrated aircraft air data system
- Patent number 5,001,638
- Issue date Mar 19, 1991
- The Boeing Company
- Ward H. Zimmerman
- G05 - CONTROLLING REGULATING
Information Patent Grant
Integrated-strapdown-air-data sensor system
- Patent number 4,303,978
- Issue date Dec 1, 1981
- The Boeing Company
- Jack C. Shaw
- G01 - MEASURING TESTING
Information Patent Grant
Gyroscope closed-loop speed controller
- Patent number 4,269,073
- Issue date May 26, 1981
- The Boeing Company
- Melville D. McIntyre
- G01 - MEASURING TESTING

Patents Applicationslast 30 patents

Information Patent Application
SYSTEMS AND METHODS FOR CONTROLLING AN AIRCRAFT USING DISSIMILAR AI...
- Publication number 20240278927
- Publication date Aug 22, 2024
- The Boeing Company
- Sherwin Chunshek Li
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ALTERNATIVE METHOD TO DETERMINE THE AIR MASS STATE OF AN AIRCRAFT A...
- Publication number 20140330455
- Publication date Nov 6, 2014
- The Boeing Company
- Melville Duncan Walter MCINTYRE
- G01 - MEASURING TESTING
Information Patent Application
Hard Landing Report Based on Sink Rate Algorithm
- Publication number 20110276217
- Publication date Nov 10, 2011
- The Boeing Company
- Daniel T. Sim
- G07 - CHECKING-DEVICES
Information Patent Application
SKIPPING FILTER FOR INERTIALLY AUGMENTED LANDING SYSTEM
- Publication number 20030083792
- Publication date May 1, 2003
- Leonard R. Anderson
- G01 - MEASURING TESTING

Melville D. McIntyre

Person

Patents Grantslast 30 patents

Alternative method to determine the air mass state of an aircraft a...

Alternative method to determine the air mass state of an aircraft a...

Airspeed sensing system for an aircraft

Apparatus and method for navigation of an aircraft

Skipping filter for inertially augmented landing system

Inertially augmented GPS landing system

Airspeed prediction filter

Integrated fault-tolerant air data inertial reference system

Integrated aircraft air data system

Integrated-strapdown-air-data sensor system

Gyroscope closed-loop speed controller

Patents Applicationslast 30 patents

SYSTEMS AND METHODS FOR CONTROLLING AN AIRCRAFT USING DISSIMILAR AI...

ALTERNATIVE METHOD TO DETERMINE THE AIR MASS STATE OF AN AIRCRAFT A...

Hard Landing Report Based on Sink Rate Algorithm

SKIPPING FILTER FOR INERTIALLY AUGMENTED LANDING SYSTEM