G05D 1/0841
To prevent a coupling between different modes
Official title: {to prevent a coupling between different modes}
G05D1/0841 (To prevent a coupling between different modes) appears on 19 US grants and 17 published applications in this corpus.
Search patents in G05D- Granted patents
- 19
- Published applications
- 17
- Assignees
- 21
- Inventors
- 42
- Latest grant
- 24 Feb 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1979 | 1 | 0 |
| 1980 | 0 | 0 |
| 1981 | 0 | 0 |
| 1982 | 0 | 0 |
| 1983 | 0 | 0 |
| 1984 | 0 | 0 |
| 1985 | 0 | 0 |
| 1986 | 1 | 0 |
| 1987 | 0 | 0 |
| 1988 | 0 | 0 |
| 1989 | 0 | 0 |
| 1990 | 0 | 0 |
| 1991 | 0 | 0 |
| 1992 | 0 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 0 | 0 |
| 1998 | 0 | 0 |
| 1999 | 0 | 0 |
| 2000 | 0 | 0 |
| 2001 | 1 | 0 |
| 2002 | 0 | 0 |
| 2003 | 1 | 1 |
| 2004 | 0 | 1 |
| 2005 | 0 | 0 |
| 2006 | 0 | 0 |
| 2007 | 2 | 1 |
| 2008 | 0 | 0 |
| 2009 | 0 | 0 |
| 2010 | 0 | 0 |
| 2011 | 0 | 1 |
| 2012 | 0 | 0 |
| 2013 | 1 | 2 |
| 2014 | 2 | 1 |
| 2015 | 1 | 0 |
| 2016 | 0 | 1 |
| 2017 | 0 | 1 |
| 2018 | 0 | 0 |
| 2019 | 1 | 1 |
| 2020 | 2 | 3 |
| 2021 | 0 | 1 |
| 2022 | 2 | 3 |
| 2023 | 2 | 0 |
| 2024 | 1 | 0 |
| 2025 | 0 | 0 |
| 2026 | 1 | 0 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Thrust vectoring for fluid borne vehicles24 Feb 2026US 12,560,942 B2Autonomous Devices Limited
- Multivariable airspeed and flight path angle control of a co-axial rotary wing aircraft with a pusher-propeller12 Nov 2024US 12,140,970 B2Lockheed Martin Corporation
- System and method for mitigating an effect of an excitation of a structural flexible mode of an aircraft19 Dec 2023US 11,845,537 B2Bombardier Inc.
- Multi-rotor aircraft and method of controlling same4 Jul 2023US 11,693,429 B2Volocopter GmbH
- Control laws for pedal-to-roll coupling23 Aug 2022US 11,422,573 B2Airbus Canada Limited Partnership
- Multivariable airspeed and flight path angle control of a co-axial rotary wing aircraft with a pusher-propeller15 Dec 2022US 2022/0397916 A1Lockheed Martin Corporation
- Thrust vectoring for fluid borne vehicles28 Jul 2022US 2022/0236746 A1Autonomous Devices Limited
- System and method for mitigating an effect of an excitation of a structural flexible mode of an aircraft24 Mar 2022US 2022/0089275 A1Bombardier Inc.
- Multi-rotor aircraft and method of controlling same25 Nov 2021US 2021/0365048 A1Volocopter GmbH
- Flight control method and device for multi-rotor unmanned aerial vehicle, and multi-rotor unmanned aerial vehicle10 Dec 2020US 2020/0387173 A1Sz Dji Technology Co., Ltd.
Most cited
By later US patents
- Speed and collective pitch bias of helicopter longitudinal cyclic pitch39US 4,168,045 AUnited Technologies Corporation · 1979
- System and method for integrating LNAV and VNAV with autopilots for existing aircraft21US 6,308,116 B1Rockwell Collins, Inc. · 2001
- Control system for an aircraft11US 10,831,192 B1Piasecki Aircraft Corporation · 2020
- Maneuver-force gradient system8US 4,563,743 AUnited Technologies Corporation · 1986
- Software controlled stiffening of flexible aircraft6US 10,279,891 B2Google Inc. · 2019