DE69206268D1 - Modellunterstüztes regelungssystem. - Google Patents
Modellunterstüztes regelungssystem.Info
- Publication number
- DE69206268D1 DE69206268D1 DE69206268T DE69206268T DE69206268D1 DE 69206268 D1 DE69206268 D1 DE 69206268D1 DE 69206268 T DE69206268 T DE 69206268T DE 69206268 T DE69206268 T DE 69206268T DE 69206268 D1 DE69206268 D1 DE 69206268D1
- Authority
- DE
- Germany
- Prior art keywords
- model
- control system
- supported control
- supported
- control
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
- G05D1/0825—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using mathematical models
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
Landscapes
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Mathematical Analysis (AREA)
- Pure & Applied Mathematics (AREA)
- Mathematical Physics (AREA)
- Mathematical Optimization (AREA)
- Algebra (AREA)
- Mechanical Engineering (AREA)
- Feedback Control In General (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/751,434 US5141177A (en) | 1991-08-28 | 1991-08-28 | Model following control system |
PCT/US1992/007236 WO1993005463A1 (en) | 1991-08-28 | 1992-08-26 | Improved model following control system |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69206268D1 true DE69206268D1 (de) | 1996-01-04 |
DE69206268T2 DE69206268T2 (de) | 1996-04-18 |
Family
ID=25021965
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69206268T Expired - Fee Related DE69206268T2 (de) | 1991-08-28 | 1992-08-26 | Modellunterstüztes regelungssystem. |
Country Status (8)
Country | Link |
---|---|
US (1) | US5141177A (de) |
EP (1) | EP0601073B1 (de) |
JP (1) | JP3420764B2 (de) |
AU (1) | AU657001B2 (de) |
CA (1) | CA2116566C (de) |
DE (1) | DE69206268T2 (de) |
ES (1) | ES2083185T3 (de) |
WO (1) | WO1993005463A1 (de) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5553817A (en) * | 1994-05-03 | 1996-09-10 | United Technologies Corporation | Turn coordination inhibit for rotary wing aircraft control system |
US5446666A (en) * | 1994-05-17 | 1995-08-29 | The Boeing Company | Ground state-fly state transition control for unique-trim aircraft flight control system |
US5596499A (en) * | 1995-02-21 | 1997-01-21 | The Boeing Company | Control law mode switching between rate command and attitude command control systems |
US5617316A (en) * | 1995-03-15 | 1997-04-01 | Sikorsky Aircraft Corporation | Maintaining attitude error constant in Euler singularity protection |
US5775303A (en) * | 1995-06-30 | 1998-07-07 | Cummins Engine Company, Inc. | High Pressure Fuel Line Connection |
US5678786A (en) * | 1995-12-06 | 1997-10-21 | Mcdonnell Douglas Helicopter Co. | Reconfigurable helicopter flight control system |
US6047226A (en) * | 1997-06-26 | 2000-04-04 | Hughes Electronics Corporation | Enhanced stellar attitude determination system |
JP3195918B2 (ja) * | 1999-03-12 | 2001-08-06 | 株式会社コミュータヘリコプタ先進技術研究所 | ヘリコプタ用飛行制御装置 |
US6330483B1 (en) | 1999-05-07 | 2001-12-11 | The Boeing Company | Optimal control system |
FR2802656B1 (fr) * | 1999-12-16 | 2002-02-15 | Eurocopter France | Systeme de commande de vol pour aeronef a voilure tournante, notamment pour helicoptere |
US6478262B1 (en) | 2001-07-17 | 2002-11-12 | Sikorsky Aircraft Corporation | Flight control system for a hybrid aircraft in the yaw axis |
US6431494B1 (en) | 2001-07-17 | 2002-08-13 | Sikorsky Aircraft Corporation | Flight control system for a hybrid aircraft in the roll axis |
FR2830630B1 (fr) * | 2001-10-05 | 2004-07-30 | Eurocopter France | Dispositif de pilotage automatique d'un helicoptere et systeme de pilotage automatique comportant un tel dispositif |
FR2876468B1 (fr) * | 2004-10-08 | 2007-08-17 | Eurocopter France | Systeme de pilotage automatique d'un helicoptere |
DE102007043328A1 (de) * | 2007-09-12 | 2009-03-19 | Endress + Hauser Process Solutions Ag | Verfahren zur Überwachung einer Prozessanlage mit einem Feldbus der Prozessautomatisierungstechnik |
US7857998B2 (en) | 2008-11-24 | 2010-12-28 | E. I. Du Pont De Nemours And Company | High conductivity polymer thick film silver conductor composition for use in RFID and other applications |
EP2261116B1 (de) * | 2009-06-09 | 2019-05-22 | Sikorsky Aircraft Corporation | Automatisches Trimmsystem für Fly-by-Wire-Flugzeuge mit einmaligen Trimmsteuerungen |
US20120209455A1 (en) * | 2011-02-10 | 2012-08-16 | Warkomski Edward J | Autopilot with Adaptive Rate/Acceleration Based Damping |
JP5893890B2 (ja) * | 2011-10-18 | 2016-03-23 | 三菱重工業株式会社 | 航空機及び航空機の制御方法 |
US10025320B2 (en) * | 2012-02-15 | 2018-07-17 | Sikorsky Aircraft Corporation | Control system for reconfigurable rotary wing aircraft |
CN105867121B (zh) * | 2016-03-28 | 2018-07-31 | 南京航空航天大学 | 用于自旋恢复的直升机非线性预测控制方法及装置 |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3057584A (en) * | 1960-03-01 | 1962-10-09 | Honeywell Regulator Co | Automatic control apparatus |
JPS5160397A (en) * | 1974-11-22 | 1976-05-26 | Kawasaki Heavy Ind Ltd | Kaitenyokukokuki niokeru jidohikoseigyosochi |
US4106094A (en) * | 1976-12-13 | 1978-08-08 | Turpin Systems Company | Strap-down attitude and heading reference system |
DE3212950C1 (de) * | 1982-04-07 | 1983-10-27 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Flugsteuerung,insbesondere fuer einen Hubschrauber |
US4527242A (en) * | 1982-06-28 | 1985-07-02 | Rockwell International Corporation | Automatic flight control pilot assist system |
AU550917B2 (en) * | 1984-04-13 | 1986-04-10 | Toshiba, Kabushiki Kaisha | Process control apparatus with reference model |
US4697768A (en) * | 1985-11-12 | 1987-10-06 | Grumman Aerospace Corporation | Flight control system employing complementary filter |
US5001646A (en) * | 1988-12-19 | 1991-03-19 | Mcdonnell Douglas Corporation | Automated helicopter flight control system |
US5008825A (en) * | 1989-05-01 | 1991-04-16 | Nadkarni Arun A | Apparatus and methods for automatically maintaining aircraft track angle |
-
1991
- 1991-08-28 US US07/751,434 patent/US5141177A/en not_active Expired - Lifetime
-
1992
- 1992-08-26 EP EP92919085A patent/EP0601073B1/de not_active Expired - Lifetime
- 1992-08-26 AU AU25063/92A patent/AU657001B2/en not_active Ceased
- 1992-08-26 ES ES92919085T patent/ES2083185T3/es not_active Expired - Lifetime
- 1992-08-26 WO PCT/US1992/007236 patent/WO1993005463A1/en active IP Right Grant
- 1992-08-26 CA CA002116566A patent/CA2116566C/en not_active Expired - Fee Related
- 1992-08-26 DE DE69206268T patent/DE69206268T2/de not_active Expired - Fee Related
- 1992-08-26 JP JP50527693A patent/JP3420764B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
AU2506392A (en) | 1993-04-05 |
ES2083185T3 (es) | 1996-04-01 |
CA2116566A1 (en) | 1993-03-18 |
AU657001B2 (en) | 1995-02-23 |
DE69206268T2 (de) | 1996-04-18 |
EP0601073A1 (de) | 1994-06-15 |
EP0601073B1 (de) | 1995-11-22 |
JPH06510006A (ja) | 1994-11-10 |
WO1993005463A1 (en) | 1993-03-18 |
US5141177A (en) | 1992-08-25 |
CA2116566C (en) | 2000-06-06 |
JP3420764B2 (ja) | 2003-06-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |