DE3881667D1 - Steuerungssystem fuer hubschrauber. - Google Patents
Steuerungssystem fuer hubschrauber.Info
- Publication number
- DE3881667D1 DE3881667D1 DE8888121089T DE3881667T DE3881667D1 DE 3881667 D1 DE3881667 D1 DE 3881667D1 DE 8888121089 T DE8888121089 T DE 8888121089T DE 3881667 T DE3881667 T DE 3881667T DE 3881667 D1 DE3881667 D1 DE 3881667D1
- Authority
- DE
- Germany
- Prior art keywords
- helicopters
- control system
- 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
-
- 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
-
- 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
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
- G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Navigation (AREA)
- Traffic Control Systems (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/135,907 US4801110A (en) | 1987-12-21 | 1987-12-21 | Approach to hover control system for helicopters |
Publications (2)
Publication Number | Publication Date |
---|---|
DE3881667D1 true DE3881667D1 (de) | 1993-07-15 |
DE3881667T2 DE3881667T2 (de) | 1993-10-07 |
Family
ID=22470307
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE88121089T Expired - Fee Related DE3881667T2 (de) | 1987-12-21 | 1988-12-16 | Steuerungssystem für Hubschrauber. |
Country Status (5)
Country | Link |
---|---|
US (1) | US4801110A (de) |
EP (1) | EP0321876B1 (de) |
JP (1) | JPH01208295A (de) |
CA (1) | CA1311034C (de) |
DE (1) | DE3881667T2 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2757939C1 (ru) * | 2020-12-29 | 2021-10-25 | Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации | Способ оценки пространственного положения воздушного судна вертолётного типа |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4924400A (en) * | 1988-09-01 | 1990-05-08 | United Technologies Corporation | Arrangement for controlling the performance of bob-up/bob-down maneuvers by a helicopter |
US5001646A (en) * | 1988-12-19 | 1991-03-19 | Mcdonnell Douglas Corporation | Automated helicopter flight control system |
US5195039A (en) * | 1990-05-03 | 1993-03-16 | United Technologies Corporation | Hover position hold system for rotary winged aircraft |
DE4420059C2 (de) * | 1994-06-08 | 2000-12-14 | Leubner Hans Peter | Start- und Landeführungssystem für Drehflügler und andere Senkrechtstarter |
US6516284B2 (en) * | 1994-11-21 | 2003-02-04 | Phatrat Technology, Inc. | Speedometer for a moving sportsman |
US7386401B2 (en) | 1994-11-21 | 2008-06-10 | Phatrat Technology, Llc | Helmet that reports impact information, and associated methods |
US7127335B2 (en) * | 2003-03-25 | 2006-10-24 | Rosemount Aerospace Inc. | Low airspeed assist algorithm for air data computer applications |
US6731234B1 (en) | 2003-06-11 | 2004-05-04 | Honeywell International Inc. | Radar anti-fade systems and methods |
US7248208B2 (en) * | 2004-06-10 | 2007-07-24 | Honeywell International Inc. | Methods and systems for maintaining a position during hovering operations |
US7284420B2 (en) | 2004-07-13 | 2007-10-23 | Honeywell International Inc. | Air data system and method for rotary aircraft |
FR2882163B1 (fr) * | 2005-02-15 | 2011-05-27 | Thales Sa | Equipement de pilotage automatique pour aeronef a voilure tournante |
US7693620B2 (en) * | 2005-05-31 | 2010-04-06 | The Boeing Company | Approach guidance system and method for airborne mobile platform |
US9235217B2 (en) * | 2005-10-03 | 2016-01-12 | Sikorsky Aircraft Corporation | Automatic dual rotor speed control for helicopters |
FR2902081B1 (fr) * | 2006-06-12 | 2008-07-11 | Airbus France Sas | Procede et dispositif d'assistance a l'atterissage pour aeronef |
US8508387B2 (en) * | 2007-05-24 | 2013-08-13 | Aviation Communication & Surveillance Systems Llc | Systems and methods for aircraft windshear detection |
EP2188179A4 (de) * | 2007-08-17 | 2016-08-03 | Sikorsky Aircraft Corp | Stabilisierte annäherung an einen punkt in einer abgeschwächten visuellen umgebung |
US8712607B2 (en) * | 2009-12-07 | 2014-04-29 | Sikorsky Aircraft Corporation | Systems and methods for velocity profile based approach to point control |
CN103314336B (zh) | 2011-01-14 | 2016-08-10 | 贝尔直升机泰克斯特龙公司 | 用于控制竖直飞行航迹的飞行控制***和方法 |
EP2710439B1 (de) * | 2011-07-15 | 2016-09-07 | Bell Helicopter Textron Inc. | Flugsteuerungsfunktionen zur automatischen schwebeflugsteuerung |
US9856017B2 (en) * | 2013-06-11 | 2018-01-02 | Bell Helicopter Textron Inc. | Torque based method of limiting vertical axis augmentation |
US9308985B2 (en) * | 2014-04-11 | 2016-04-12 | Sikorsky Aircraft Corporation | Deceleration to hover modulation |
FR3036497B1 (fr) * | 2015-05-19 | 2017-06-16 | Airbus Operations Sas | Procede et systeme de gestion de donnees d'un radioaltimetre d'aeronef. |
US10642283B2 (en) | 2016-10-07 | 2020-05-05 | Sikorsky Aircraft Corporation | Simultaneous flight path control and attitude control with control axis splitting |
US10654561B2 (en) * | 2017-02-02 | 2020-05-19 | Textron Innovations Inc. | Rotorcraft fly-by-wire go-around mode |
US10101749B1 (en) * | 2017-03-21 | 2018-10-16 | Bell Helicopter Textron Inc. | Combined airspeed and inertial data for rotorcraft longitudinal control |
US20190039720A1 (en) * | 2017-08-07 | 2019-02-07 | Bell Helicopter Textron Inc. | System and Method for Rotorcraft Approach to Hover |
US11352900B2 (en) | 2019-05-14 | 2022-06-07 | Pratt & Whitney Canada Corp. | Method and system for operating a rotorcraft engine |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2830291A (en) * | 1954-09-23 | 1958-04-08 | Sperry Rand Corp | Flare-out control |
US3126474A (en) * | 1960-12-19 | 1964-03-24 | Flight path angle | |
US3627238A (en) * | 1969-05-29 | 1971-12-14 | Lear Siegler Inc | Speed command generation system for vertical descent control |
US3665465A (en) * | 1969-10-22 | 1972-05-23 | Rita Ann Miller | Deceleration schedule for aircraft landing |
US3927306A (en) * | 1974-03-29 | 1975-12-16 | Sperry Rand Corp | Helicopter flight path control |
US4354237A (en) * | 1980-06-24 | 1982-10-12 | The Boeing Company | Method and apparatus for producing an aircraft flare path control signal |
US4740899A (en) * | 1982-07-01 | 1988-04-26 | Rockwell International Corporation | Use of headwind and airspeed to achieve a transition to a hover in a helicopter or vtol aircraft |
US4551804A (en) * | 1983-02-08 | 1985-11-05 | Sperry Corporation | Approach to hover control system for helicopters |
US4628455A (en) * | 1983-05-06 | 1986-12-09 | Sperry Corporation | Cross axis torque limiter for helicopter autopilot |
-
1987
- 1987-12-21 US US07/135,907 patent/US4801110A/en not_active Expired - Lifetime
-
1988
- 1988-12-16 DE DE88121089T patent/DE3881667T2/de not_active Expired - Fee Related
- 1988-12-16 EP EP88121089A patent/EP0321876B1/de not_active Expired - Lifetime
- 1988-12-19 CA CA000586296A patent/CA1311034C/en not_active Expired - Fee Related
- 1988-12-21 JP JP63323166A patent/JPH01208295A/ja active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2757939C1 (ru) * | 2020-12-29 | 2021-10-25 | Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации | Способ оценки пространственного положения воздушного судна вертолётного типа |
Also Published As
Publication number | Publication date |
---|---|
DE3881667T2 (de) | 1993-10-07 |
EP0321876B1 (de) | 1993-06-09 |
JPH01208295A (ja) | 1989-08-22 |
EP0321876A2 (de) | 1989-06-28 |
US4801110A (en) | 1989-01-31 |
CA1311034C (en) | 1992-12-01 |
EP0321876A3 (en) | 1990-06-13 |
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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 |