DE60037048D1 - System zur Vermeidung von Heckberührung bei Flugzeugen - Google Patents
System zur Vermeidung von Heckberührung bei FlugzeugenInfo
- Publication number
- DE60037048D1 DE60037048D1 DE60037048T DE60037048T DE60037048D1 DE 60037048 D1 DE60037048 D1 DE 60037048D1 DE 60037048 T DE60037048 T DE 60037048T DE 60037048 T DE60037048 T DE 60037048T DE 60037048 D1 DE60037048 D1 DE 60037048D1
- Authority
- DE
- Germany
- Prior art keywords
- aircraft
- end contact
- avoiding rear
- avoiding
- contact
- 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 - Lifetime
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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
-
- 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
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)
- Traffic Control Systems (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US16878399P | 1999-12-02 | 1999-12-02 | |
US168783P | 1999-12-02 | ||
US520329 | 2000-03-07 | ||
US09/520,329 US6422517B1 (en) | 1999-12-02 | 2000-03-07 | Aircraft tailstrike avoidance system |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60037048D1 true DE60037048D1 (de) | 2007-12-20 |
DE60037048T2 DE60037048T2 (de) | 2008-07-10 |
Family
ID=26864448
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60037048T Expired - Lifetime DE60037048T2 (de) | 1999-12-02 | 2000-11-30 | System zur Vermeidung von Heckberührung bei Flugzeugen |
DE60033236T Expired - Lifetime DE60033236T2 (de) | 1999-12-02 | 2000-11-30 | Flugsteuersysteme, welche einen Schutz gegen einen versehentlichen Heckbodenkontakt bereitstellen |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60033236T Expired - Lifetime DE60033236T2 (de) | 1999-12-02 | 2000-11-30 | Flugsteuersysteme, welche einen Schutz gegen einen versehentlichen Heckbodenkontakt bereitstellen |
Country Status (5)
Country | Link |
---|---|
US (2) | US6422517B1 (de) |
EP (1) | EP1235712B1 (de) |
AU (1) | AU3789701A (de) |
DE (2) | DE60037048T2 (de) |
WO (1) | WO2001040051A2 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107102646A (zh) * | 2016-02-22 | 2017-08-29 | 波音公司 | 防止飞行器尾部接触地面的系统和方法 |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6897803B2 (en) * | 2003-06-11 | 2005-05-24 | Honeywell International Inc. | Radar altimeter with forward ranging capabilities |
US20050216131A1 (en) * | 2004-03-24 | 2005-09-29 | Sodemann Wesley C | Residential load power management system |
US6980153B2 (en) * | 2004-05-17 | 2005-12-27 | Honeywell International Inc. | Radar altimeter for helicopter load carrying operations |
US7239266B2 (en) * | 2004-08-26 | 2007-07-03 | Honeywell International Inc. | Radar altimeter |
US20060089759A1 (en) * | 2004-10-22 | 2006-04-27 | Honeywell International Inc. | Systems and methods for performing high accurate distance measuring for radar altimeters |
US7751976B2 (en) * | 2005-08-26 | 2010-07-06 | Sikorsky Aircraft Corporation | Rotary wing aircraft flight control system with a proximity cueing and avoidance system |
US8165733B2 (en) * | 2007-09-04 | 2012-04-24 | Embraer S.A. | Stall, buffeting, low speed and high attitude protection system |
US7681086B2 (en) * | 2007-09-20 | 2010-03-16 | Embraer- Empresa Brasileira De Aeronautica S.A. | Fault tree map generation |
US8532848B2 (en) * | 2010-10-19 | 2013-09-10 | Honeywell International Inc. | Systems and methods for alerting potential tailstrike during landing |
US8793040B2 (en) * | 2011-06-10 | 2014-07-29 | Embraer S.A. | Climb-optimized auto takeoff system |
US8774985B2 (en) * | 2011-07-22 | 2014-07-08 | The Boeing Company | Systems and methods for generating a command trajectory |
US8742973B1 (en) * | 2011-09-22 | 2014-06-03 | Rockwell Collins, Inc. | System and method of determining increased turbulence susceptibility with elapsed flight time |
US8781653B2 (en) * | 2012-01-11 | 2014-07-15 | The Boeing Company | Quiet landing attitude modifier for airplane |
US8866667B2 (en) | 2012-02-22 | 2014-10-21 | Honeywell International Inc. | High sensitivity single antenna FMCW radar |
US9828113B2 (en) | 2013-11-05 | 2017-11-28 | Safe Flight Instrument Corporation | Tailstrike warning system |
WO2015069228A1 (en) * | 2013-11-05 | 2015-05-14 | Safe Flight Instrument Corporation | Tailstrike warning system |
US9546003B2 (en) | 2014-03-14 | 2017-01-17 | Safe Flight Instrument Corporation | Deflare pitch command |
US9660605B2 (en) | 2014-06-12 | 2017-05-23 | Honeywell International Inc. | Variable delay line using variable capacitors in a maximally flat time delay filter |
US10018716B2 (en) | 2014-06-26 | 2018-07-10 | Honeywell International Inc. | Systems and methods for calibration and optimization of frequency modulated continuous wave radar altimeters using adjustable self-interference cancellation |
US20170008639A1 (en) | 2015-07-08 | 2017-01-12 | Safe Flight Instrument Corporation | Aircraft turbulence detection |
US11226639B2 (en) | 2016-09-23 | 2022-01-18 | Yaborã Indústria Aeronáutica S.A. | Enhanced take-off system |
CN106586004A (zh) * | 2016-12-05 | 2017-04-26 | 中国航空工业集团公司洛阳电光设备研究所 | 一种飞机着陆擦尾告警方法 |
US10816998B2 (en) | 2017-09-18 | 2020-10-27 | The Boeing Company | Airplane takeoff trims utilizing both stabilizers and elevators |
US10852747B2 (en) * | 2018-02-21 | 2020-12-01 | The Boeing Company | Tailstrike awareness system |
CN110554712A (zh) * | 2019-10-22 | 2019-12-10 | 深圳市道通智能航空技术有限公司 | 无人机航向角初值选取方法、装置及无人机 |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3963197A (en) | 1971-12-16 | 1976-06-15 | Messerschmitt-Bolkow-Blohm Gmbh | Control device for avoiding the pitching up of missiles or aircraft |
US3979717A (en) * | 1974-06-03 | 1976-09-07 | United Technologies Corporation | Helicopter warning system |
US3945590A (en) | 1975-01-23 | 1976-03-23 | Sperry Rand Corporation | Semi-automatic takeoff control system for aircraft |
US4495483A (en) * | 1981-04-30 | 1985-01-22 | Sundstrand Corporation | Ground proximity warning system with time based mode switching |
DE3228557A1 (de) * | 1982-07-30 | 1984-02-09 | Ulrich 8000 München Trampnau | Warnvorrichtung fuer hubschrauber |
US4763266A (en) | 1982-12-27 | 1988-08-09 | The Boeing Company | Aircraft flight command and display system |
US4769645A (en) * | 1983-06-10 | 1988-09-06 | Sundstrand Data Control, Inc. | Excessive pitch attitude warning system for rotary wing aircraft |
GB8327731D0 (en) * | 1983-10-17 | 1983-11-16 | Trampnau U | Warning device for helicopters |
US5224664A (en) | 1991-07-22 | 1993-07-06 | United Technologies Corporation | Adaptive control system input limiting |
FR2711257B1 (fr) | 1993-10-14 | 1995-12-22 | Aerospatiale | Système de commande de vol électrique pour avion avec protection en assiette au décollage. |
US5826834A (en) * | 1994-10-19 | 1998-10-27 | Honeywell Inc. | Self adaptive limiter for automatic control of approach and landing |
US5823479A (en) * | 1996-05-20 | 1998-10-20 | The Boeing Company | Landing attitude modifier for airplane |
US5901927A (en) * | 1996-07-18 | 1999-05-11 | Honeywell Inc. | Ground strike protection function for aircraft autopilot |
US6121899A (en) * | 1999-04-16 | 2000-09-19 | Rockwell Collins, Inc. | Impending aircraft tail strike warning display symbology |
-
2000
- 2000-03-07 US US09/520,329 patent/US6422517B1/en not_active Expired - Lifetime
- 2000-11-30 WO PCT/US2000/032862 patent/WO2001040051A2/en active IP Right Grant
- 2000-11-30 EP EP00992006A patent/EP1235712B1/de not_active Expired - Lifetime
- 2000-11-30 AU AU37897/01A patent/AU3789701A/en not_active Abandoned
- 2000-11-30 DE DE60037048T patent/DE60037048T2/de not_active Expired - Lifetime
- 2000-11-30 DE DE60033236T patent/DE60033236T2/de not_active Expired - Lifetime
-
2002
- 2002-01-08 US US10/043,401 patent/US6761336B2/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107102646A (zh) * | 2016-02-22 | 2017-08-29 | 波音公司 | 防止飞行器尾部接触地面的系统和方法 |
Also Published As
Publication number | Publication date |
---|---|
DE60033236D1 (de) | 2007-03-22 |
US6422517B1 (en) | 2002-07-23 |
AU3789701A (en) | 2001-06-12 |
US20020066829A1 (en) | 2002-06-06 |
EP1235712A2 (de) | 2002-09-04 |
WO2001040051A3 (en) | 2001-10-25 |
DE60033236T2 (de) | 2007-11-15 |
EP1235712B1 (de) | 2007-01-31 |
DE60037048T2 (de) | 2008-07-10 |
US6761336B2 (en) | 2004-07-13 |
WO2001040051A2 (en) | 2001-06-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8339 | Ceased/non-payment of the annual fee | ||
8370 | Indication related to discontinuation of the patent is to be deleted | ||
8363 | Opposition against the patent |