ATE356972T1 - Verfahren, vorrichtung und computerprogrammprodukt zur geländeanzeige in drehflügelflugzeugen - Google Patents
Verfahren, vorrichtung und computerprogrammprodukt zur geländeanzeige in drehflügelflugzeugenInfo
- Publication number
- ATE356972T1 ATE356972T1 AT01950254T AT01950254T ATE356972T1 AT E356972 T1 ATE356972 T1 AT E356972T1 AT 01950254 T AT01950254 T AT 01950254T AT 01950254 T AT01950254 T AT 01950254T AT E356972 T1 ATE356972 T1 AT E356972T1
- Authority
- AT
- Austria
- Prior art keywords
- computer program
- program product
- rotary wing
- wing aircraft
- terrain display
- Prior art date
Links
- 238000004590 computer program Methods 0.000 title abstract 2
- 238000000034 method Methods 0.000 title abstract 2
Classifications
-
- 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
- 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
-
- 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
- G05D1/0646—Rate of change of altitude or depth specially adapted for aircraft to follow the profile of undulating ground
-
- 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)
- 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)
- Navigation (AREA)
- Emergency Alarm Devices (AREA)
- Alarm Systems (AREA)
- Nozzles (AREA)
- Toys (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US20774000P | 2000-05-26 | 2000-05-26 | |
| US20799800P | 2000-05-26 | 2000-05-26 | |
| US20751500P | 2000-05-26 | 2000-05-26 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE356972T1 true ATE356972T1 (de) | 2007-04-15 |
Family
ID=27395072
Family Applications (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT01950254T ATE356972T1 (de) | 2000-05-26 | 2001-05-25 | Verfahren, vorrichtung und computerprogrammprodukt zur geländeanzeige in drehflügelflugzeugen |
| AT01961604T ATE426144T1 (de) | 2000-05-26 | 2001-05-25 | Vorrichtung, verfahren und computerprogrammprodukt fur ein erweitertes hubschrauber-bodennaherungswarnsystem |
| AT01958827T ATE426145T1 (de) | 2000-05-26 | 2001-05-25 | Vorrichtung, verfahren und computerprogrammprodukt fur ein hubschrauber- bodennaherungswarnsystem |
Family Applications After (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT01961604T ATE426144T1 (de) | 2000-05-26 | 2001-05-25 | Vorrichtung, verfahren und computerprogrammprodukt fur ein erweitertes hubschrauber-bodennaherungswarnsystem |
| AT01958827T ATE426145T1 (de) | 2000-05-26 | 2001-05-25 | Vorrichtung, verfahren und computerprogrammprodukt fur ein hubschrauber- bodennaherungswarnsystem |
Country Status (5)
| Country | Link |
|---|---|
| EP (3) | EP1285227B1 (de) |
| JP (1) | JP2003534987A (de) |
| AT (3) | ATE356972T1 (de) |
| DE (3) | DE60138015D1 (de) |
| WO (3) | WO2001092823A2 (de) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8078344B2 (en) * | 2005-04-21 | 2011-12-13 | Honeywell International Inc. | System and method for displaying the protected airspace associated with a circle-to-land maneuver |
| FR2897839B1 (fr) * | 2006-02-27 | 2009-01-23 | Airbus France Sas | Procede et dispositif d'ajustememnt automatique d'une image d'un ecran de navigation d'aeronef. |
| US8098176B2 (en) * | 2010-05-07 | 2012-01-17 | Honeywell International Inc. | Systems and methods for adjusting landing gear alert envelope for offshore platforms and building-top landings |
| FR2999156B1 (fr) * | 2012-12-12 | 2015-01-16 | Thales Sa | Procede de securisation d'un aeronef |
| CN103354041B (zh) * | 2013-06-25 | 2015-12-09 | 上海交通大学 | 一种民用飞机地形感知与告警系统模式四告警包线生成方法 |
| US9685091B2 (en) * | 2013-08-30 | 2017-06-20 | Insitu, Inc. | Aerial vehicle awareness display |
| US9511880B2 (en) | 2015-03-31 | 2016-12-06 | Honeywell International Inc. | Flight deck display systems and methods for generating vertical speed alerts during steep approaches of rotary wing aircraft |
| WO2017173416A1 (en) * | 2016-03-31 | 2017-10-05 | Netjets Inc. | Aviation sector special departure procedure systems and methods |
| FR3063715B1 (fr) | 2017-03-09 | 2019-04-12 | Dassault Aviation | Systeme d'avertissement de proximite au sol d'un aeronef, avionique et procede associe |
| CN109903590B (zh) * | 2017-12-11 | 2023-04-07 | 上海航空电器有限公司 | 一种基于地形包线的航空器自动机动规避方法 |
| FR3090978B1 (fr) * | 2018-12-19 | 2020-12-04 | Airbus Helicopters | procédé de détection de la proximité d’un arrangement latérale d’un aéronef avec le sol et aéronef |
| US11908335B2 (en) | 2022-07-13 | 2024-02-20 | Honeywell International Inc. | System and method for suggesting switching operational modes of a ground proximity warning system |
| WO2024034134A1 (ja) * | 2022-08-12 | 2024-02-15 | 株式会社Subaru | 航空機 |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4980684A (en) * | 1983-06-10 | 1990-12-25 | Sundstrand Data Controls, Inc. | Warning system for tactical rotary wing aircraft |
| US5839080B1 (en) * | 1995-07-31 | 2000-10-17 | Allied Signal Inc | Terrain awareness system |
| US6043759A (en) * | 1996-07-29 | 2000-03-28 | Alliedsignal | Air-ground logic system and method for rotary wing aircraft |
| DE19831452C1 (de) * | 1998-07-14 | 2000-03-09 | Eurocopter Deutschland | Verfahren zur Unterstützung der Flugführung |
-
2001
- 2001-05-25 WO PCT/US2001/017179 patent/WO2001092823A2/en not_active Ceased
- 2001-05-25 AT AT01950254T patent/ATE356972T1/de not_active IP Right Cessation
- 2001-05-25 EP EP01950254A patent/EP1285227B1/de not_active Expired - Lifetime
- 2001-05-25 DE DE60138015T patent/DE60138015D1/de not_active Expired - Lifetime
- 2001-05-25 JP JP2002500188A patent/JP2003534987A/ja not_active Withdrawn
- 2001-05-25 WO PCT/US2001/017228 patent/WO2001090694A2/en not_active Ceased
- 2001-05-25 DE DE60127250T patent/DE60127250T2/de not_active Expired - Lifetime
- 2001-05-25 AT AT01961604T patent/ATE426144T1/de not_active IP Right Cessation
- 2001-05-25 AT AT01958827T patent/ATE426145T1/de not_active IP Right Cessation
- 2001-05-25 EP EP01961604A patent/EP1285228B1/de not_active Expired - Lifetime
- 2001-05-25 EP EP01958827A patent/EP1290407B1/de not_active Expired - Lifetime
- 2001-05-25 WO PCT/US2001/017105 patent/WO2001090693A2/en not_active Ceased
- 2001-05-25 DE DE60138017T patent/DE60138017D1/de not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| DE60127250D1 (de) | 2007-04-26 |
| EP1290407B1 (de) | 2009-03-18 |
| EP1290407A2 (de) | 2003-03-12 |
| JP2003534987A (ja) | 2003-11-25 |
| WO2001090694A3 (en) | 2002-04-18 |
| DE60127250T2 (de) | 2007-12-06 |
| WO2001092823A2 (en) | 2001-12-06 |
| WO2001092823A3 (en) | 2002-05-23 |
| EP1285227B1 (de) | 2007-03-14 |
| EP1285228A2 (de) | 2003-02-26 |
| DE60138017D1 (de) | 2009-04-30 |
| WO2001090693A2 (en) | 2001-11-29 |
| ATE426144T1 (de) | 2009-04-15 |
| EP1285228B1 (de) | 2009-03-18 |
| EP1285227A2 (de) | 2003-02-26 |
| WO2001090693A3 (en) | 2002-04-18 |
| WO2001090694A2 (en) | 2001-11-29 |
| ATE426145T1 (de) | 2009-04-15 |
| DE60138015D1 (de) | 2009-04-30 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |