DE3275665D1 - Aircraft flight control system - Google Patents
Aircraft flight control systemInfo
- Publication number
- DE3275665D1 DE3275665D1 DE8282107195T DE3275665T DE3275665D1 DE 3275665 D1 DE3275665 D1 DE 3275665D1 DE 8282107195 T DE8282107195 T DE 8282107195T DE 3275665 T DE3275665 T DE 3275665T DE 3275665 D1 DE3275665 D1 DE 3275665D1
- Authority
- DE
- Germany
- Prior art keywords
- control system
- flight control
- aircraft flight
- aircraft
- flight
- 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
Links
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 title 1
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
- G05D1/04—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)
- Feedback Control In General (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/301,911 US4419732A (en) | 1981-09-14 | 1981-09-14 | Method and apparatus for an aircraft inner loop elevator control system |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3275665D1 true DE3275665D1 (en) | 1987-04-16 |
Family
ID=23165419
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8282107195T Expired DE3275665D1 (en) | 1981-09-14 | 1982-08-09 | Aircraft flight control system |
Country Status (3)
Country | Link |
---|---|
US (1) | US4419732A (de) |
EP (1) | EP0074493B1 (de) |
DE (1) | DE3275665D1 (de) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5036469A (en) * | 1989-03-02 | 1991-07-30 | The Boeing Company | Pitch attitude command flight control system for landing flare |
US5377937A (en) * | 1991-09-03 | 1995-01-03 | The Boeing Company | Aircraft flare control system utilizing an envelope limiter |
US5901927A (en) * | 1996-07-18 | 1999-05-11 | Honeywell Inc. | Ground strike protection function for aircraft autopilot |
US6809099B2 (en) * | 2000-11-03 | 2004-10-26 | President And Fellows Of Harvard College | Saframycins, analogues and uses thereof |
US6676088B1 (en) * | 2002-10-07 | 2004-01-13 | Safe Flight Instrument Corporation | Flare control system |
US7183054B2 (en) * | 2003-06-03 | 2007-02-27 | President And Fellows Of Harvard College | Assay for identifying biological targets of polynucleotide-binding compounds |
CA2568848C (en) * | 2004-07-16 | 2013-06-25 | Airbus France | Method and device for improving maneuverability of an aircraft during approach phases before landing followed by flare-out |
US8019492B2 (en) * | 2007-10-26 | 2011-09-13 | The Boeing Company | Operator fine tracking assist using sensor derived inputs |
US8275496B2 (en) | 2007-11-21 | 2012-09-25 | The Boeing Company | Longitudinal and vertical gust feed forward compensation using lateral control surfaces |
US8781653B2 (en) * | 2012-01-11 | 2014-07-15 | The Boeing Company | Quiet landing attitude modifier for airplane |
US10816998B2 (en) | 2017-09-18 | 2020-10-27 | The Boeing Company | Airplane takeoff trims utilizing both stabilizers and elevators |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3447765A (en) * | 1965-05-27 | 1969-06-03 | Bendix Corp | Automatic control system for landing an aircraft |
US3291421A (en) * | 1965-09-20 | 1966-12-13 | Lear Siegler Inc | Pitch controller for automatic landing |
US3333795A (en) * | 1966-01-10 | 1967-08-01 | Collins Radio Co | Flare computer |
US3523663A (en) * | 1968-03-28 | 1970-08-11 | Bendix Corp | Terminal flare controller |
US3601339A (en) * | 1968-06-03 | 1971-08-24 | Elliott Brothers London Ltd | Aircraft-landing systems |
US3604908A (en) * | 1969-05-19 | 1971-09-14 | Sperry Rand Corp | Landing control system for aircraft |
US3578269A (en) * | 1969-06-11 | 1971-05-11 | Lear Siegler Inc | Automatic flare and altitude hold system |
US3626163A (en) * | 1970-01-28 | 1971-12-07 | Us Army | Automatic landing system |
US3652835A (en) * | 1970-05-14 | 1972-03-28 | Sperry Rand Corp | Aircraft glide slope coupler system |
US3847328A (en) * | 1972-01-31 | 1974-11-12 | Boeing Co | Automatic go-around control system for aircraft |
US3801049A (en) * | 1972-01-31 | 1974-04-02 | Boeing Co | Automatic approach landing and go-around pitch axis control system for aircraft |
US4006871A (en) * | 1972-06-19 | 1977-02-08 | The Boeing Company | Automatic pitch axis control system for aircraft |
US4164340A (en) * | 1973-03-19 | 1979-08-14 | The Boeing Company | Method and apparatus for determining when a glide slope signal exceeds a predetermined level |
US3892373A (en) * | 1973-12-07 | 1975-07-01 | Bendix Corp | Integrated glide path/flare automatic flight control system |
US3887148A (en) * | 1973-12-19 | 1975-06-03 | Sperry Rand Corp | Aircraft glide slope coupler and landing system |
US3918662A (en) * | 1974-01-21 | 1975-11-11 | Boeing Co | Localizer lateral guidance control system |
US3976267A (en) * | 1974-11-14 | 1976-08-24 | The Boeing Company | Vertical glide slope control system including complementary filter |
US4032093A (en) * | 1975-06-27 | 1977-06-28 | The Boeing Company | Adaptive energy management for vertical speed control of an aircraft |
US4104612A (en) * | 1977-02-03 | 1978-08-01 | Mcdonnell Douglas Corporation | Head-up display command bar generator |
US4141522A (en) * | 1977-05-16 | 1979-02-27 | Boeing Commercial Airplane Company | Independent glide slope gain programming system |
US4357661A (en) * | 1980-02-22 | 1982-11-02 | The Boeing Company | Aircraft landing control system |
US4326253A (en) * | 1980-03-31 | 1982-04-20 | The Boeing Company | Lift control system for aircraft vertical path guidance |
US4354237A (en) * | 1980-06-24 | 1982-10-12 | The Boeing Company | Method and apparatus for producing an aircraft flare path control signal |
-
1981
- 1981-09-14 US US06/301,911 patent/US4419732A/en not_active Expired - Lifetime
-
1982
- 1982-08-09 DE DE8282107195T patent/DE3275665D1/de not_active Expired
- 1982-08-09 EP EP82107195A patent/EP0074493B1/de not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US4419732A (en) | 1983-12-06 |
EP0074493A1 (de) | 1983-03-23 |
EP0074493B1 (de) | 1987-03-11 |
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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 |