GB9308295D0 - Method of piloting an aircraft in order to avoid its colliding with the ground - Google Patents
Method of piloting an aircraft in order to avoid its colliding with the groundInfo
- Publication number
- GB9308295D0 GB9308295D0 GB939308295A GB9308295A GB9308295D0 GB 9308295 D0 GB9308295 D0 GB 9308295D0 GB 939308295 A GB939308295 A GB 939308295A GB 9308295 A GB9308295 A GB 9308295A GB 9308295 D0 GB9308295 D0 GB 9308295D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- piloting
- colliding
- aircraft
- ground
- avoid
- 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.)
- Withdrawn
Links
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- 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
- G05D1/0646—Rate of change of altitude or depth specially adapted for aircraft to follow the profile of undulating ground
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/005—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 with correlation of navigation data from several sources, e.g. map or contour matching
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C5/00—Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels
- G01C5/005—Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels altimeters for aircraft
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9205090A FR2690518B1 (en) | 1992-04-24 | 1992-04-24 | METHOD OF PILOTING AN AIRCRAFT TO AVOID COLLISION WITH THE GROUND. |
Publications (2)
Publication Number | Publication Date |
---|---|
GB9308295D0 true GB9308295D0 (en) | 1993-06-09 |
GB2266286A GB2266286A (en) | 1993-10-27 |
Family
ID=9429243
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9308295A Withdrawn GB2266286A (en) | 1992-04-24 | 1993-04-22 | Method of piloting an aircraft to avoid its colliding with the ground. |
Country Status (4)
Country | Link |
---|---|
CA (1) | CA2094627A1 (en) |
DE (1) | DE4313403A1 (en) |
FR (1) | FR2690518B1 (en) |
GB (1) | GB2266286A (en) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6292721B1 (en) | 1995-07-31 | 2001-09-18 | Allied Signal Inc. | Premature descent into terrain visual awareness enhancement to EGPWS |
US6606034B1 (en) | 1995-07-31 | 2003-08-12 | Honeywell International Inc. | Terrain awareness system |
US5839080B1 (en) * | 1995-07-31 | 2000-10-17 | Allied Signal Inc | Terrain awareness system |
US6691004B2 (en) | 1995-07-31 | 2004-02-10 | Honeywell International, Inc. | Method for determining a currently obtainable climb gradient of an aircraft |
US6138060A (en) * | 1995-07-31 | 2000-10-24 | Alliedsignal Inc. | Terrain awareness system |
US6092009A (en) * | 1995-07-31 | 2000-07-18 | Alliedsignal | Aircraft terrain information system |
DE19528954C2 (en) * | 1995-08-07 | 2000-04-13 | Eurocopter Deutschland | Display device for displaying flight guidance information |
GB2310184B (en) * | 1996-02-19 | 2000-10-11 | Marconi Gec Ltd | Aircraft terrain advisory system |
US5864307A (en) * | 1996-02-19 | 1999-01-26 | Gec Marconi Limited | Aircraft terrain advisory system |
FR2747492B1 (en) * | 1996-04-15 | 1998-06-05 | Dassault Electronique | TERRAIN ANTI-COLLISION DEVICE FOR AIRCRAFT WITH TURN PREDICTION |
US6043759A (en) * | 1996-07-29 | 2000-03-28 | Alliedsignal | Air-ground logic system and method for rotary wing aircraft |
US5781126A (en) * | 1996-07-29 | 1998-07-14 | Alliedsignal Inc. | Ground proximity warning system and methods for rotary wing aircraft |
DE19709097C2 (en) * | 1997-03-06 | 1999-02-04 | Dornier Gmbh | Flight guidance system for low-flying aircraft |
WO2000048159A2 (en) | 1999-02-01 | 2000-08-17 | Honeywell International Inc. | Apparatus, methods and computer program product for the generation and use of a runway field clearance floor envelope about a selected runway |
WO2000045126A1 (en) | 1999-02-01 | 2000-08-03 | Honeywell International Inc. | Ground proximity warning system |
DE60030413T2 (en) | 1999-02-01 | 2007-09-13 | Honeywell International Inc. | A method, apparatus and computer program products for determining a corrected distance between an aircraft and a selected runway |
WO2000047948A1 (en) | 1999-02-01 | 2000-08-17 | Honeywell International Inc. | Apparatus, method, and computer program product for generating terrain clearance floor envelopes about a selected runway |
US6734808B1 (en) | 1999-10-05 | 2004-05-11 | Honeywell International Inc. | Method, apparatus and computer program products for alerting submersible vessels to hazardous conditions |
US6469664B1 (en) | 1999-10-05 | 2002-10-22 | Honeywell International Inc. | Method, apparatus, and computer program products for alerting surface vessels to hazardous conditions |
IT1316577B1 (en) * | 2000-11-08 | 2003-04-24 | Claudio Bianchini | ANTI-COLLISION DEVICE FOR TRANSPORT VEHICLES USING LECOORDINATE GPS AND ITS OPERATING SYSTEM. |
DE10308913A1 (en) * | 2003-02-28 | 2004-09-30 | Ais Advanced Infodata Systems Gmbh | Aircraft safety system uses a data representation of the earth's surface in which a high resolution data mesh provides position and height data |
FR2870606B1 (en) * | 2004-05-18 | 2010-10-08 | Airbus France | METHOD AND DEVICE FOR SECURING A LOW ALTITUDE FLIGHT OF AN AIRCRAFT |
DE102019103173A1 (en) | 2019-02-08 | 2020-08-13 | Volocopter Gmbh | Method and system for movement planning for aircraft, in particular for load-carrying and / or person-carrying VTOL aircraft |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2043388B (en) * | 1979-02-09 | 1983-08-17 | Boeing Co | Minimum safe altitude monitoring indicating and warning system |
US4646244A (en) * | 1984-02-02 | 1987-02-24 | Sundstrand Data Control, Inc. | Terrain advisory system |
DE3604401A1 (en) * | 1986-02-12 | 1987-08-20 | Messerschmitt Boelkow Blohm | LOW FLY PROCEDURE FOR AUTOMATIC COURSE DETERMINATION |
-
1992
- 1992-04-24 FR FR9205090A patent/FR2690518B1/en not_active Expired - Lifetime
-
1993
- 1993-04-22 GB GB9308295A patent/GB2266286A/en not_active Withdrawn
- 1993-04-22 CA CA002094627A patent/CA2094627A1/en not_active Abandoned
- 1993-04-23 DE DE4313403A patent/DE4313403A1/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
DE4313403A1 (en) | 1993-10-28 |
FR2690518B1 (en) | 1997-01-03 |
GB2266286A (en) | 1993-10-27 |
CA2094627A1 (en) | 1993-10-25 |
FR2690518A1 (en) | 1993-10-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |