by acting on the pitch

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G05D1/0623

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Parent Industries

GPHYSICS G05Controlling systems G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES G05D1/00Control of position, course or altitude of land, water, air, or space vehicles

Current Industry

G05D1/0623by acting on the pitch

Industries

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Patents Grantslast 30 patents

Information Patent Grant
Process and machine for load alleviation
- Patent number 11,834,152
- Issue date Dec 5, 2023
- The Boeing Company
- Alexander C. Ho
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Flying object takeoff control system
- Patent number 11,618,595
- Issue date Apr 4, 2023
- Toyota Jidosha Kabushiki Kaisha
- Nobuhiro Okuno
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Process and machine for load alleviation
- Patent number 11,535,364
- Issue date Dec 27, 2022
- The Boeing Company
- Alexander C. Ho
- G05 - CONTROLLING REGULATING
Information Patent Grant
Machine learning based airflow sensing for aircraft
- Patent number 11,119,504
- Issue date Sep 14, 2021
- International Business Machines Corporation
- Wang Zhou
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Grant
Method and system for determining a vertical trajectory of an aircraft
- Patent number 10,109,202
- Issue date Oct 23, 2018
- Dassault Aviation
- Eric Boulle
- G08 - SIGNALLING
Information Patent Grant
Hover attitude trim for vehicle
- Patent number 9,964,960
- Issue date May 8, 2018
- Sikorsky Aircraft Corporation
- Cody Fegely
- G05 - CONTROLLING REGULATING
Information Patent Grant
Method and apparatus for minimizing dynamic structural loads of an...
- Patent number 9,446,837
- Issue date Sep 20, 2016
- EADS Deutschland GmbH
- Andreas Wildschek
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method and apparatus for minimizing dynamic structural loads of an...
- Patent number 9,242,723
- Issue date Jan 26, 2016
- EADS Deutschland GmbH
- Andreas Wildschek
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Automatic pilot pitch angle compensation
- Patent number 9,058,040
- Issue date Jun 16, 2015
- The Boeing Company
- Frederick Charles Henry Blechen
- G05 - CONTROLLING REGULATING
Information Patent Grant
Longitudinal and vertical gust feed forward compensation using late...
- Patent number 8,706,321
- Issue date Apr 22, 2014
- The Boeing Company
- Brian K. Rupnik
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method and device for attenuating on an aircraft the effects of a v...
- Patent number 8,359,130
- Issue date Jan 22, 2013
- Airbus Operations SAS
- Alexandre Colomer
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Longitudinal and vertical gust feed forward compensation using late...
- Patent number 8,275,496
- Issue date Sep 25, 2012
- The Boeing Company
- Brian K. Rupnik
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method and device for reducing on an aircraft lateral effects of a...
- Patent number 8,219,266
- Issue date Jul 10, 2012
- Airbus Operations SAS
- Stephane Puig
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method and device for reducing on an aircraft the effects of a vert...
- Patent number 8,190,306
- Issue date May 29, 2012
- Airbus Operations SAS
- Stephane Puig
- G05 - CONTROLLING REGULATING
Information Patent Grant
Control system for automatic flight in windshear conditions
- Patent number 8,170,730
- Issue date May 1, 2012
- Textron Innovations Inc.
- Shyhpyng Jack Shue
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method and device for dynamically alleviating loads generated on an...
- Patent number 8,000,845
- Issue date Aug 16, 2011
- Airbus France
- Nathalie Fabre-Raimbault
- G05 - CONTROLLING REGULATING
Information Patent Grant
Control system for automatic flight in windshear conditions
- Patent number 8,000,847
- Issue date Aug 16, 2011
- Textron Innovations Inc.
- Shyhpyng Jack Shue
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Active pitch control method and device for an aircraft
- Patent number 7,853,369
- Issue date Dec 14, 2010
- Airbus France
- Fabrice Villaume
- G05 - CONTROLLING REGULATING
Information Patent Grant
Method for ensuring the safety of an aircraft flying horizontally a...
- Patent number 7,422,176
- Issue date Sep 9, 2008
- Airbus France
- Stéphane Chardon
- G05 - CONTROLLING REGULATING
Information Patent Grant
System and method for compensating structural vibrations of an airc...
- Patent number 6,416,017
- Issue date Jul 9, 2002
- DaimlerChrysler AG
- Juergen Becker
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Control of the height of guidable flying bodies
- Patent number 6,042,049
- Issue date Mar 28, 2000
- Short Brothers PLC
- James W. McIlroy
- G05 - CONTROLLING REGULATING
Information Patent Grant
Method and device for detecting vertical gusts of wind and applicat...
- Patent number 5,995,880
- Issue date Nov 30, 1999
- Aerospatiale Societe Nationale Industrielle
- Panxika Larramendy
- G05 - CONTROLLING REGULATING
Information Patent Grant
Windshear guidance system
- Patent number 5,361,065
- Issue date Nov 1, 1994
- Honeywell Inc.
- David A. Johnson
- G05 - CONTROLLING REGULATING
Information Patent Grant
TCAS II pitch guidance control law and display symbol
- Patent number 5,248,968
- Issue date Sep 28, 1993
- The Boeing Company
- Brian D. Kelly
- G08 - SIGNALLING
Information Patent Grant
Pitch guidance system
- Patent number 5,136,518
- Issue date Aug 4, 1992
- Sundstrand Data Control, Inc.
- J. Howard Glover
- G05 - CONTROLLING REGULATING
Information Patent Grant
Path capture forcing function generator for aircraft vertical axis...
- Patent number 5,117,362
- Issue date May 26, 1992
- Honeywell
- Roger D. Peckham
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Speed reference system for piloting an aircraft
- Patent number 4,967,363
- Issue date Oct 30, 1990
- Aerospatiale Societe Nationale Industrielle
- Jean L. Bonafe
- G05 - CONTROLLING REGULATING
Information Patent Grant
Universal-type gust alleviation system for aircraft
- Patent number 4,905,934
- Issue date Mar 6, 1990
- Grumman Aerospace Corporation
- Jimmie Chin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Optimal flight guidance for aircraft in windshear
- Patent number 4,863,120
- Issue date Sep 5, 1989
- Honeywell Inc.
- Terry L. Zweifel
- G05 - CONTROLLING REGULATING
Information Patent Grant
Flight control system and method
- Patent number 4,849,900
- Issue date Jul 18, 1989
- The Boeing Company
- James D. Blight
- G05 - CONTROLLING REGULATING

Patents Applicationslast 30 patents

Information Patent Application
Aircraft, Aircraft Control Method, and Computer Readable Storage Me...
- Publication number 20230350430
- Publication date Nov 2, 2023
- Hanwang Technology Co., Ltd.
- Jing Liu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
DUAL AGENT REINFORCEMENT LEARNING BASED SYSTEM FOR AUTONOMOUS OPERA...
- Publication number 20230025154
- Publication date Jan 26, 2023
- The Boeing Company
- Prabhat KUMAR
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
FLYING OBJECT TAKEOFF CONTROL SYSTEM
- Publication number 20220035381
- Publication date Feb 3, 2022
- Toyota Jidosha Kabushiki Kaisha
- Nobuhiro OKUNO
- G05 - CONTROLLING REGULATING
Information Patent Application
METHOD, DEVICE, AND SYSTEM FOR ADJUSTING ATTITUDE OF A DEVICE AND C...
- Publication number 20200097026
- Publication date Mar 26, 2020
- SZ DJI Technology Co., Ltd.
- Zhuo GUO
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Control System for Automatic Flight in Windshear Conditions
- Publication number 20110282523
- Publication date Nov 17, 2011
- Shyhpyng Jack Shue
- G05 - CONTROLLING REGULATING
Information Patent Application
AUTOMATIC PILOT PITCH ANGLE COMPENSATION
- Publication number 20100222944
- Publication date Sep 2, 2010
- Frederick Charles Henry Blechen
- G05 - CONTROLLING REGULATING
Information Patent Application
METHOD AND DEVICE FOR REDUCING ON AN AIRCRAFT LATERAL EFFECTS OF A...
- Publication number 20100070114
- Publication date Mar 18, 2010
- AIRBUS FRANCE
- Stephane PUIG
- G05 - CONTROLLING REGULATING
Information Patent Application
ACTIVE PITCH CONTROL METHOD AND DEVICE FOR AN AIRCRAFT
- Publication number 20100042270
- Publication date Feb 18, 2010
- AIRBUS FRANCE
- Fabrice VILLAUME
- G05 - CONTROLLING REGULATING
Information Patent Application
METHOD AND DEVICE FOR REDUCING ON AN AIRCRAFT THE EFFECTS OF A VERT...
- Publication number 20090314900
- Publication date Dec 24, 2009
- AIRBUS FRANCE
- Stephane PUIG
- G05 - CONTROLLING REGULATING
Information Patent Application
LONGITUDINAL AND VERTICAL GUST FEED FORWARD COMPENSATION USING LATE...
- Publication number 20090132104
- Publication date May 21, 2009
- The Boeing Company
- BRIAN K. RUPNIK
- G05 - CONTROLLING REGULATING
Information Patent Application
METHOD AND DEVICE FOR DYNAMICALLY ALLEVIATING LOADS GENERATED ON AN...
- Publication number 20080265104
- Publication date Oct 30, 2008
- AIRBUS FRANCE
- Nathalie Fabre-Raimbault
- G05 - CONTROLLING REGULATING
Information Patent Application
Method and Device for Attenuating on an Aircraft the Effects of a V...
- Publication number 20080251648
- Publication date Oct 16, 2008
- AIRBUS FRANCE
- Alexandre Colomer
- G05 - CONTROLLING REGULATING
Information Patent Application
Control System for Automatic Flight in Windshear Conditions
- Publication number 20080046137
- Publication date Feb 21, 2008
- Shyhpyng Jack Shue
- G05 - CONTROLLING REGULATING
Information Patent Application
Method for ensuring the safety of an aircraft flying horizontally a...
- Publication number 20050269448
- Publication date Dec 8, 2005
- AIRBUS FRANCE
- Stephane Chardon
- G05 - CONTROLLING REGULATING

by acting on the pitch

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Process and machine for load alleviation

Flying object takeoff control system

Process and machine for load alleviation

Machine learning based airflow sensing for aircraft

Method and system for determining a vertical trajectory of an aircraft

Hover attitude trim for vehicle

Method and apparatus for minimizing dynamic structural loads of an...

Method and apparatus for minimizing dynamic structural loads of an...

Automatic pilot pitch angle compensation

Longitudinal and vertical gust feed forward compensation using late...

Method and device for attenuating on an aircraft the effects of a v...

Longitudinal and vertical gust feed forward compensation using late...

Method and device for reducing on an aircraft lateral effects of a...

Method and device for reducing on an aircraft the effects of a vert...

Control system for automatic flight in windshear conditions

Method and device for dynamically alleviating loads generated on an...

Control system for automatic flight in windshear conditions

Active pitch control method and device for an aircraft

Method for ensuring the safety of an aircraft flying horizontally a...

System and method for compensating structural vibrations of an airc...

Control of the height of guidable flying bodies

Method and device for detecting vertical gusts of wind and applicat...

Windshear guidance system

TCAS II pitch guidance control law and display symbol

Pitch guidance system

Path capture forcing function generator for aircraft vertical axis...

Speed reference system for piloting an aircraft

Universal-type gust alleviation system for aircraft

Optimal flight guidance for aircraft in windshear

Flight control system and method

Patents Applicationslast 30 patents

Aircraft, Aircraft Control Method, and Computer Readable Storage Me...

DUAL AGENT REINFORCEMENT LEARNING BASED SYSTEM FOR AUTONOMOUS OPERA...

FLYING OBJECT TAKEOFF CONTROL SYSTEM

METHOD, DEVICE, AND SYSTEM FOR ADJUSTING ATTITUDE OF A DEVICE AND C...

Control System for Automatic Flight in Windshear Conditions

AUTOMATIC PILOT PITCH ANGLE COMPENSATION

METHOD AND DEVICE FOR REDUCING ON AN AIRCRAFT LATERAL EFFECTS OF A...

ACTIVE PITCH CONTROL METHOD AND DEVICE FOR AN AIRCRAFT

METHOD AND DEVICE FOR REDUCING ON AN AIRCRAFT THE EFFECTS OF A VERT...

LONGITUDINAL AND VERTICAL GUST FEED FORWARD COMPENSATION USING LATE...

METHOD AND DEVICE FOR DYNAMICALLY ALLEVIATING LOADS GENERATED ON AN...

Method and Device for Attenuating on an Aircraft the Effects of a V...

Control System for Automatic Flight in Windshear Conditions

Method for ensuring the safety of an aircraft flying horizontally a...