to prevent a coupling between different modes

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CPC
G05D1/0841

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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

G05D1/0841to prevent a coupling between different modes

Industries

Patents Grantslast 30 patents

Information Patent Grant
Control laws for pedal-to-roll coupling
- Patent number 11,422,573
- Issue date Aug 23, 2022
- BOMBARDIER INC.
- Matthew Olsthoorn
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Grant
Software controlled stiffening of flexible aircraft
- Patent number 10,279,891
- Issue date May 7, 2019
- Google LLC
- Mark Krebs
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Yaw damping system and method for aircraft
- Patent number 8,874,286
- Issue date Oct 28, 2014
- Textron Innovations, Inc.
- Steven G. Hagerott
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Yaw damping system and method for aircraft
- Patent number 8,620,492
- Issue date Dec 31, 2013
- Textron Innovations Inc.
- Steven G. Hagerott
- G05 - CONTROLLING REGULATING
Information Patent Grant
Device and method for damping at least one of a rigid body mode and...
- Patent number 7,258,307
- Issue date Aug 21, 2007
- Airbus Deutschland GmbH
- Michael Enzinger
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method and device for detecting pilot induced oscillations in an ai...
- Patent number 7,225,061
- Issue date May 29, 2007
- Airbus France
- Nathalie Raimbault
- G05 - CONTROLLING REGULATING
Information Patent Grant
System and method for controlling an aircraft
- Patent number 6,641,086
- Issue date Nov 4, 2003
- Northrop Grumman Corporation
- Walter D. Clark
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
System and method for integrating LNAV and VNAV with autopilots for...
- Patent number 6,308,116
- Issue date Oct 23, 2001
- Rockwell Collins
- Ralph D. Ricks
- G05 - CONTROLLING REGULATING
Information Patent Grant
Maneuver-force gradient system
- Patent number 4,563,743
- Issue date Jan 7, 1986
- United Technologies Corporation
- Richard D. Murphy
- G05 - CONTROLLING REGULATING
Information Patent Grant
Speed and collective pitch bias of helicopter longitudinal cyclic p...
- Patent number 4,168,045
- Issue date Sep 18, 1979
- United Technologies Corporation
- Gregory P. Wright
- G05 - CONTROLLING REGULATING
Information Patent Grant
3752420
- Patent number 3,752,420
- Issue date Aug 14, 1973
- G05 - CONTROLLING REGULATING
Information Patent Grant
3075729
- Patent number 3,075,729
- Issue date Jan 29, 1963
- G05 - CONTROLLING REGULATING
Information Patent Grant
3072370
- Patent number 3,072,370
- Issue date Jan 8, 1963
- G05 - CONTROLLING REGULATING
Information Patent Grant
3058697
- Patent number 3,058,697
- Issue date Oct 16, 1962
- G05 - CONTROLLING REGULATING
Information Patent Grant
2967031
- Patent number 2,967,031
- Issue date Jan 3, 1961
- G05 - CONTROLLING REGULATING
Information Patent Grant
2964269
- Patent number 2,964,269
- Issue date Dec 13, 1960
- G05 - CONTROLLING REGULATING
Information Patent Grant
2953326
- Patent number 2,953,326
- Issue date Sep 20, 1960
- G05 - CONTROLLING REGULATING
Information Patent Grant
2868481
- Patent number 2,868,481
- Issue date Jan 13, 1959
- G05 - CONTROLLING REGULATING
Information Patent Grant
2834562
- Patent number 2,834,562
- Issue date May 13, 1958
- G05 - CONTROLLING REGULATING
Information Patent Grant
2832552
- Patent number 2,832,552
- Issue date Apr 29, 1958
- G05 - CONTROLLING REGULATING
Information Patent Grant
2827250
- Patent number 2,827,250
- Issue date Mar 18, 1958
- G05 - CONTROLLING REGULATING

Patents Applicationslast 30 patents

Information Patent Application
THRUST VECTORING FOR FLUID BORNE VEHICLES
- Publication number 20220236746
- Publication date Jul 28, 2022
- Autonomous Devices Limited
- Ken Wahren
- G05 - CONTROLLING REGULATING
Information Patent Application
FLIGHT CONTROL METHOD AND DEVICE FOR MULTI-ROTOR UNMANNED AERIAL VE...
- Publication number 20200387173
- Publication date Dec 10, 2020
- SZ DJI Technology Co., Ltd.
- Jiadi WANG
- G05 - CONTROLLING REGULATING
Information Patent Application
CONTROL LAWS FOR PEDAL-TO-ROLL COUPLING
- Publication number 20190204855
- Publication date Jul 4, 2019
- Bombardier Inc.
- Matthew OLSTHOORN
- G05 - CONTROLLING REGULATING
Information Patent Application
Yaw Damping System And Method For Aircraft
- Publication number 20140114505
- Publication date Apr 24, 2014
- TEXTRON INNOVATIONS INC.
- Steven G. Hagerott
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Yaw Damping System And Method For Aircraft
- Publication number 20130226374
- Publication date Aug 29, 2013
- CESSNA AIRCRAFT COMPANY
- Steven G. Hagerott
- G05 - CONTROLLING REGULATING
Information Patent Application
METHOD FOR PROVIDING A PILOT WARNING SIGNAL FOR A PILOT OF AN AIRCR...
- Publication number 20110273314
- Publication date Nov 10, 2011
- Hans-Gerd Giesseler
- G05 - CONTROLLING REGULATING
Information Patent Application
Device and method for dampening at least one of a rigid body mode a...
- Publication number 20070018053
- Publication date Jan 25, 2007
- Michael Enzinger
- G05 - CONTROLLING REGULATING
Information Patent Application
Method and device for detecting pilot induced oscillations in an ai...
- Publication number 20040098176
- Publication date May 20, 2004
- Nathalie Raimbault
- G05 - CONTROLLING REGULATING
Information Patent Application
System and method for controlling an aircraft
- Publication number 20030034421
- Publication date Feb 20, 2003
- Northrop Grumman Corporation
- Walter D. Clark
- G05 - CONTROLLING REGULATING

to prevent a coupling between different modes

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Control laws for pedal-to-roll coupling

Software controlled stiffening of flexible aircraft

Yaw damping system and method for aircraft

Yaw damping system and method for aircraft

Device and method for damping at least one of a rigid body mode and...

Method and device for detecting pilot induced oscillations in an ai...

System and method for controlling an aircraft

System and method for integrating LNAV and VNAV with autopilots for...

Maneuver-force gradient system

Speed and collective pitch bias of helicopter longitudinal cyclic p...

3752420

3075729

3072370

3058697

2967031

2964269

2953326

2868481

2834562

2832552

2827250

Patents Applicationslast 30 patents

THRUST VECTORING FOR FLUID BORNE VEHICLES

FLIGHT CONTROL METHOD AND DEVICE FOR MULTI-ROTOR UNMANNED AERIAL VE...

CONTROL LAWS FOR PEDAL-TO-ROLL COUPLING

Yaw Damping System And Method For Aircraft

Yaw Damping System And Method For Aircraft

METHOD FOR PROVIDING A PILOT WARNING SIGNAL FOR A PILOT OF AN AIRCR...

Device and method for dampening at least one of a rigid body mode a...

Method and device for detecting pilot induced oscillations in an ai...

System and method for controlling an aircraft