DE69222536D1 - Koordinierte kursabweichung bei niedrigen geschwindigkeiten für drehflügelflugzeug - Google Patents
Koordinierte kursabweichung bei niedrigen geschwindigkeiten für drehflügelflugzeugInfo
- Publication number
- DE69222536D1 DE69222536D1 DE69222536T DE69222536T DE69222536D1 DE 69222536 D1 DE69222536 D1 DE 69222536D1 DE 69222536 T DE69222536 T DE 69222536T DE 69222536 T DE69222536 T DE 69222536T DE 69222536 D1 DE69222536 D1 DE 69222536D1
- Authority
- DE
- Germany
- Prior art keywords
- low speed
- rotating wing
- wing plane
- course difference
- coordinated
- 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
-
- 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
- G05D1/085—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability to ensure coordination between different movements
-
- 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)
- Automation & Control Theory (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Feedback Control In General (AREA)
- Toys (AREA)
- Retarders (AREA)
- Control Of Multiple Motors (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/751,436 US5213283A (en) | 1991-08-28 | 1991-08-28 | Low speed turn coordination for rotary wing aircraft |
PCT/US1992/006436 WO1993005460A1 (en) | 1991-08-28 | 1992-07-31 | Low speed turn coordination for rotary wing aircraft |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69222536D1 true DE69222536D1 (de) | 1997-11-06 |
DE69222536T2 DE69222536T2 (de) | 1998-02-05 |
Family
ID=25021975
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69222536T Expired - Fee Related DE69222536T2 (de) | 1991-08-28 | 1992-07-31 | Koordinierte kursabweichung bei niedrigen geschwindigkeiten für drehflügelflugzeug |
Country Status (10)
Country | Link |
---|---|
US (1) | US5213283A (de) |
EP (1) | EP0601016B1 (de) |
JP (1) | JP3308531B2 (de) |
KR (1) | KR100244834B1 (de) |
AU (1) | AU657359B2 (de) |
CA (1) | CA2114551C (de) |
DE (1) | DE69222536T2 (de) |
ES (1) | ES2110517T3 (de) |
IL (1) | IL102970A (de) |
WO (1) | WO1993005460A1 (de) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5238203A (en) * | 1991-08-28 | 1993-08-24 | United Technologies Corporation | High speed turn coordination for rotary wing aircraft |
US5553817A (en) * | 1994-05-03 | 1996-09-10 | United Technologies Corporation | Turn coordination inhibit for rotary wing aircraft control system |
US5617316A (en) * | 1995-03-15 | 1997-04-01 | Sikorsky Aircraft Corporation | Maintaining attitude error constant in Euler singularity protection |
US5799768A (en) * | 1996-07-17 | 1998-09-01 | Compunetics, Inc. | Coin identification apparatus |
JP3166703B2 (ja) * | 1998-03-27 | 2001-05-14 | 双葉電子工業株式会社 | 遠隔制御ヘリコプタ用ジャイロ装置 |
US6076024A (en) * | 1998-04-29 | 2000-06-13 | Sikorsky Aircraft Corporation | Earth-referenced wind adjustment for hovering aircraft |
US6648269B2 (en) | 2001-12-10 | 2003-11-18 | Sikorsky Aircraft Corporation | Trim augmentation system for a rotary wing aircraft |
US7706932B2 (en) * | 2006-11-30 | 2010-04-27 | Instituto Nacional de Tecnica Aeroespacial “Estaban Terradas” | Method for controlling control parameters in an air vehicle and system of controlling an air vehicle |
US7970498B2 (en) * | 2007-06-01 | 2011-06-28 | Sikorsky Aircraft Corporation | Model based sensor system for loads aware control laws |
EP2635942B1 (de) | 2011-01-14 | 2015-06-17 | Bell Helicopter Textron Inc. | Flugsteuerungsrichtlinien für vertikale flugroutensteuerung |
FR2981045B1 (fr) * | 2011-10-10 | 2013-10-25 | Eurocopter France | Systeme de pilotage en lacet pour giravion, mettant en oeuvre un organe entraine par l'homme qui genere des commandes de vol par objectif |
US10025320B2 (en) * | 2012-02-15 | 2018-07-17 | Sikorsky Aircraft Corporation | Control system for reconfigurable rotary wing aircraft |
US9360869B1 (en) | 2013-12-03 | 2016-06-07 | Sikorsky Aircraft Corporation | Vehicle heading error compensation |
FR3023017B1 (fr) | 2014-06-30 | 2016-06-10 | Airbus Helicopters | Systeme et procede de commande de vol d'un aeronef a voilure tournante en tenue de trajectoire ou tenue de cap selon sa vitesse d'avancement |
FR3023018B1 (fr) | 2014-06-30 | 2016-06-10 | Airbus Helicopters | Procede et systeme de mise en vol stationnaire d'un aeronef a voilure tournante en tenue de trajectoire ou tenue de cap selon sa vitesse d'avancement |
FR3023016B1 (fr) | 2014-06-30 | 2016-07-01 | Airbus Helicopters | Systeme et procede de commande de vol en tenue de trajectoire pour un aeronef a voilure tournante |
EP3201077B1 (de) | 2014-10-01 | 2020-05-20 | Sikorsky Aircraft Corporation | Doppelrotor, drehflügelflugzeug |
WO2016053408A1 (en) | 2014-10-01 | 2016-04-07 | Sikorsky Aircraft Corporation | Acoustic signature variation of aircraft utilizing a clutch |
FR3030760B1 (fr) | 2014-12-18 | 2017-12-22 | Airbus Helicopters | Procede et systeme de determination d'une vitesse angulaire en virage pour un aeronef a voilure tournante |
US10024187B2 (en) | 2015-03-20 | 2018-07-17 | General Electric Company | Gas turbine engine health determination |
FR3036805B1 (fr) | 2015-05-28 | 2018-06-29 | Airbus Helicopters | Procede de determination de la vitesse air longitudinale et de la vitesse sol longitudinale d'un aeronef a voiture tournante selon son exposition au vent |
US10642283B2 (en) * | 2016-10-07 | 2020-05-05 | Sikorsky Aircraft Corporation | Simultaneous flight path control and attitude control with control axis splitting |
US11299259B2 (en) * | 2020-01-29 | 2022-04-12 | Textron Innovations Inc. | Hybrid low speed control |
DE102020107456A1 (de) * | 2020-03-18 | 2021-09-23 | Volocopter Gmbh | Verfahren und Steuergerät zur Kurvenkoordinierung eines Fluggerätes sowie ein Fluggerät mit Kurvenkoordinierung |
US11479349B2 (en) * | 2020-12-01 | 2022-10-25 | Textron Innovations Inc. | Tail rotor balancing systems for use on rotorcraft |
US20230290256A1 (en) * | 2022-03-09 | 2023-09-14 | Lockheed Martin Corporation | Controlling aircraft to avoid terrain obstacles using reduced order closed loop models |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3057584A (en) * | 1960-03-01 | 1962-10-09 | Honeywell Regulator Co | Automatic control apparatus |
US3688099A (en) * | 1971-04-28 | 1972-08-29 | Lear Siegler Inc | Automatic control system with a digital computer |
US4067517A (en) * | 1976-02-03 | 1978-01-10 | United Technologies Corporation | Automatic heading synchronization control system |
US4003532A (en) * | 1976-03-15 | 1977-01-18 | United Technologies Corporation | Heading hold logic |
US4106094A (en) * | 1976-12-13 | 1978-08-08 | Turpin Systems Company | Strap-down attitude and heading reference system |
US4206891A (en) * | 1978-10-26 | 1980-06-10 | United Technologies Corporation | Helicopter pedal feel force proportional to side slip |
US4312039A (en) * | 1980-01-24 | 1982-01-19 | Sperry Corporation | Transient free synchronization system |
US4313201A (en) * | 1980-03-05 | 1982-01-26 | United Technologies Corporation | Tested, dissimilar helicopter stability augmentation |
US4382283A (en) * | 1980-08-08 | 1983-05-03 | United Technologies Corporation | Helicopter attitude and airspeed acquisition and retention system |
US4477876A (en) * | 1981-03-30 | 1984-10-16 | United Technologies Corporation | Dual response aircraft reference synchronization |
US4371939A (en) * | 1981-03-30 | 1983-02-01 | United Technologies Corporation | Roll attitude inhibit of aircraft coordinated turn disengagement |
US4484283A (en) * | 1981-03-30 | 1984-11-20 | United Technologies Corporation | Aircraft roll-yaw fault protocols |
US4392203A (en) * | 1981-03-30 | 1983-07-05 | United Technologies Corporation | Aircraft coordinated turn with lagged roll rate |
US4626998A (en) * | 1983-05-02 | 1986-12-02 | United Technologies Corporation | Heading reference trim system |
US5001646A (en) * | 1988-12-19 | 1991-03-19 | Mcdonnell Douglas Corporation | Automated helicopter flight control system |
US5023796A (en) * | 1989-10-03 | 1991-06-11 | Honeywell, Inc. | Flight control apparatus with predictive heading/track hold command |
US5238203A (en) * | 1991-08-28 | 1993-08-24 | United Technologies Corporation | High speed turn coordination for rotary wing aircraft |
-
1991
- 1991-08-28 US US07/751,436 patent/US5213283A/en not_active Expired - Lifetime
-
1992
- 1992-07-31 JP JP50518293A patent/JP3308531B2/ja not_active Expired - Fee Related
- 1992-07-31 DE DE69222536T patent/DE69222536T2/de not_active Expired - Fee Related
- 1992-07-31 WO PCT/US1992/006436 patent/WO1993005460A1/en active IP Right Grant
- 1992-07-31 AU AU24744/92A patent/AU657359B2/en not_active Ceased
- 1992-07-31 ES ES92918348T patent/ES2110517T3/es not_active Expired - Lifetime
- 1992-07-31 KR KR1019940700621A patent/KR100244834B1/ko not_active IP Right Cessation
- 1992-07-31 CA CA002114551A patent/CA2114551C/en not_active Expired - Fee Related
- 1992-07-31 EP EP92918348A patent/EP0601016B1/de not_active Expired - Lifetime
- 1992-08-27 IL IL10297092A patent/IL102970A/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
AU2474492A (en) | 1993-04-05 |
JP3308531B2 (ja) | 2002-07-29 |
IL102970A0 (en) | 1993-02-21 |
EP0601016A1 (de) | 1994-06-15 |
AU657359B2 (en) | 1995-03-09 |
ES2110517T3 (es) | 1998-02-16 |
WO1993005460A1 (en) | 1993-03-18 |
CA2114551A1 (en) | 1993-03-18 |
CA2114551C (en) | 1998-05-05 |
EP0601016B1 (de) | 1997-10-01 |
JPH06510003A (ja) | 1994-11-10 |
IL102970A (en) | 1996-05-14 |
KR100244834B1 (ko) | 2000-02-15 |
US5213283A (en) | 1993-05-25 |
DE69222536T2 (de) | 1998-02-05 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE69222536D1 (de) | Koordinierte kursabweichung bei niedrigen geschwindigkeiten für drehflügelflugzeug | |
DE69205172T2 (de) | Koordinierte Kursabweichung bei hohen Geschwindigkeiten für Drehflügelflugzeug. | |
DE69123382T2 (de) | Geschwindigkeitsregler für Massen | |
DE69204071T2 (de) | Modellunterstütze Geschwindigkeitsteuerung bei niedrigen Geschwindigkeiten für Drehflügelflugzeug. | |
DK159384D0 (da) | Ergocalciferolderivater | |
DK35384D0 (da) | Vinylcephalosporin-derivater | |
DK20884D0 (da) | Phenothiazonderivater | |
DK221384D0 (da) | Isoindolderivater | |
DE3471299D1 (de) | Oxamic-acid derivatives | |
DE3464610D1 (de) | 2-alkylthiopenem derivatives | |
DK354684A (da) | Azol-dioxolan-derivater | |
DK346984A (da) | Formamidoximderivater | |
DE3477197D1 (de) | 2-azacycloalkylthiopenem derivatives | |
DE69709486T2 (de) | Horizontalgeschwindigkeitsanzeiger für Drehflügel-Luftfahrzeug | |
FR2555587B1 (fr) | Derives de 14-des(hydroxymethyl)-mycaminosyltylonolide | |
DK163470C (da) | Hoejhastigheds-halvledermultiplexer | |
DE3476803D1 (de) | Furane-3-carboxylic-acid derivatives | |
DE3472258D1 (de) | Thiodeazapurine derivatives | |
DE69301364T2 (de) | Visiervorrichtung für Drehflügelflugzeug | |
KR890021685U (ko) | 테이프 속도 조정장치 | |
BR8307679A (pt) | Derivados de pirano | |
DK414684A (da) | Diphenylsulfid-derivater | |
DE3464902D1 (de) | 2-bromo-1-tetralone derivatives | |
DE3473268D1 (de) | 5-fluorouracilnitroxylderivatives | |
ES274573Y (es) | Magnetoviscosimetro multivariante de gradiente de velocidad variable |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |