DE2139075C2 - Vorrichtung zur Ermittlung eines Bodenabstandsignals und eines Höhenänderungssignales eines Flugzeuges - Google Patents
Vorrichtung zur Ermittlung eines Bodenabstandsignals und eines Höhenänderungssignales eines FlugzeugesInfo
- Publication number
- DE2139075C2 DE2139075C2 DE2139075A DE2139075A DE2139075C2 DE 2139075 C2 DE2139075 C2 DE 2139075C2 DE 2139075 A DE2139075 A DE 2139075A DE 2139075 A DE2139075 A DE 2139075A DE 2139075 C2 DE2139075 C2 DE 2139075C2
- Authority
- DE
- Germany
- Prior art keywords
- signal
- aircraft
- altitude
- ground
- warning
- 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
- 230000008859 change Effects 0.000 title claims description 90
- 230000000295 complement effect Effects 0.000 claims description 18
- 238000013459 approach Methods 0.000 claims description 9
- 230000009194 climbing Effects 0.000 claims description 8
- 230000001133 acceleration Effects 0.000 claims description 6
- 238000000034 method Methods 0.000 claims description 5
- 238000012546 transfer Methods 0.000 claims description 5
- 230000007774 longterm Effects 0.000 claims description 4
- 230000008569 process Effects 0.000 claims description 3
- 230000005484 gravity Effects 0.000 claims description 2
- 238000012545 processing Methods 0.000 claims description 2
- 230000035484 reaction time Effects 0.000 claims description 2
- 238000005259 measurement Methods 0.000 description 34
- 239000003990 capacitor Substances 0.000 description 7
- 238000010586 diagram Methods 0.000 description 5
- 230000001788 irregular Effects 0.000 description 3
- 230000035515 penetration Effects 0.000 description 3
- 230000035945 sensitivity Effects 0.000 description 3
- 230000003321 amplification Effects 0.000 description 2
- 238000009795 derivation Methods 0.000 description 2
- 238000001514 detection method Methods 0.000 description 2
- 230000004069 differentiation Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000001914 filtration Methods 0.000 description 2
- 230000024703 flight behavior Effects 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 238000003199 nucleic acid amplification method Methods 0.000 description 2
- 230000002123 temporal effect Effects 0.000 description 2
- 230000001960 triggered effect Effects 0.000 description 2
- 230000006399 behavior Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 239000002689 soil Substances 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P3/00—Measuring linear or angular speed; Measuring differences of linear or angular speeds
- G01P3/62—Devices characterised by the determination or the variation of atmospheric pressure with height to measure the vertical components of speed
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P1/00—Details of instruments
- G01P1/07—Indicating devices, e.g. for remote indication
- G01P1/08—Arrangements of scales, pointers, lamps or acoustic indicators, e.g. in automobile speedometers
- G01P1/10—Arrangements of scales, pointers, lamps or acoustic indicators, e.g. in automobile speedometers for indicating predetermined speeds
- G01P1/103—Arrangements of scales, pointers, lamps or acoustic indicators, e.g. in automobile speedometers for indicating predetermined speeds by comparing the value of the measured signal with one or several reference values
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S13/06—Systems determining position data of a target
- G01S13/08—Systems for measuring distance only
- G01S13/10—Systems for measuring distance only using transmission of interrupted, pulse modulated waves
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Radar Systems Or Details Thereof (AREA)
- Traffic Control Systems (AREA)
- Navigation (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US6286170A | 1970-08-11 | 1970-08-11 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DE2139075A1 DE2139075A1 (de) | 1972-02-17 |
| DE2139075C2 true DE2139075C2 (de) | 1982-12-16 |
Family
ID=22045317
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE2139075A Expired DE2139075C2 (de) | 1970-08-11 | 1971-08-04 | Vorrichtung zur Ermittlung eines Bodenabstandsignals und eines Höhenänderungssignales eines Flugzeuges |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US3715718A (https=) |
| JP (1) | JPS5427640B1 (https=) |
| AU (1) | AU465701B2 (https=) |
| CA (1) | CA959577A (https=) |
| DE (1) | DE2139075C2 (https=) |
| FR (1) | FR2102182B1 (https=) |
| GB (1) | GB1352531A (https=) |
| SE (1) | SE379584B (https=) |
Families Citing this family (75)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3936797A (en) * | 1974-05-28 | 1976-02-03 | Intercontinental Dynamics Corporation | Radar-barometric altitude indicator |
| US3979717A (en) * | 1974-06-03 | 1976-09-07 | United Technologies Corporation | Helicopter warning system |
| US3988713A (en) * | 1974-06-19 | 1976-10-26 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning instrument |
| US3946358A (en) | 1974-06-19 | 1976-03-23 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning instrument |
| US3936796A (en) * | 1974-06-19 | 1976-02-03 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning instrument |
| US3944968A (en) * | 1974-11-01 | 1976-03-16 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning system having speed versus altitude compensation |
| US3947808A (en) * | 1975-01-13 | 1976-03-30 | Sundstrand Data Control, Inc. | Excessive descent rate warning system for aircraft |
| US3947810A (en) * | 1975-01-13 | 1976-03-30 | Sundstrand Data Control, Inc. | Negative climb rate after take-off warning system with predetermined loss of altitude inhibit |
| US3934221A (en) * | 1975-03-06 | 1976-01-20 | Sundstrand Data Control, Inc. | Terrain closure warning system with altitude rate signal conditioning |
| US3958219A (en) * | 1975-03-06 | 1976-05-18 | Sundstrand Data Control, Inc. | Terrain closure warning system with altitude rate signal conditioning |
| US4027838A (en) * | 1975-03-18 | 1977-06-07 | United Technologies Corporation | Helicopter warning system |
| US4012626A (en) * | 1975-04-18 | 1977-03-15 | Sperry Rand Corporation | Vertical navigation control system |
| US4016565A (en) * | 1975-09-15 | 1977-04-05 | Rockwell International Corporation | Aircraft ground closure rate filtering method and means |
| US4012713A (en) * | 1975-11-05 | 1977-03-15 | Safe Flight Instrument Corporation | System for providing an indication of wind shear |
| US4135143A (en) * | 1976-06-14 | 1979-01-16 | Intercontinental Dynamics Corporation | Aircraft altitude annunciator |
| US4071894A (en) * | 1976-06-28 | 1978-01-31 | Rockwell International Corporation | Profile warning generator with anticipation of warning condition |
| FR2343223A1 (fr) * | 1976-07-01 | 1977-09-30 | Trt Telecom Radio Electr | Filtrage des alarmes dans un systeme de surveillance de la proximite du sol |
| US4093938A (en) * | 1976-10-18 | 1978-06-06 | Intercontinental Dynamics Corp. | Aircraft altitude annunciator |
| US4215334A (en) * | 1978-02-09 | 1980-07-29 | Sundstrand Data Control, Inc. | Aircraft excessive descent rate warning system |
| US4189777A (en) * | 1978-05-01 | 1980-02-19 | The Bendix Corporation | Ground proximity warning system with means for altering warning threshold in accordance with wind shear |
| FR2466751A1 (fr) * | 1979-10-03 | 1981-04-10 | Trt Telecom Radio Electr | Systeme d'aide a l'atterrissage et au vol en formation pour helicopteres |
| US4319218A (en) * | 1980-01-04 | 1982-03-09 | Sundstrand Corporation | Negative climb after take-off warning system with configuration warning means |
| US4495483A (en) * | 1981-04-30 | 1985-01-22 | Sundstrand Corporation | Ground proximity warning system with time based mode switching |
| US4433323A (en) * | 1982-02-04 | 1984-02-21 | Sundstrand Data Control, Inc. | Ground proximity warning system with time and altitude based mode switching |
| US4684948A (en) * | 1983-07-08 | 1987-08-04 | Sundstrand Data Control, Inc. | Ground proximity warning system having modified terrain closure rate warning on glide slope approach |
| US4567483A (en) * | 1982-12-10 | 1986-01-28 | Sundstrand Data Control, Inc. | Position based ground proximity warning system for aircraft |
| US4609988A (en) * | 1983-03-17 | 1986-09-02 | Sperry Corporation | Automatic prediction and capture of a preselected altitude for aircraft |
| US5001476A (en) * | 1983-05-13 | 1991-03-19 | Sundstrand Data Control, Inc. | Warning system for tactical aircraft |
| CA1241082A (en) * | 1983-05-13 | 1988-08-23 | Everette E. Vermilion | Warning system for tactical aircraft |
| IL68737A0 (en) * | 1983-05-20 | 1984-06-29 | Israel Aircraft Ind Ltd | Excessive ground-closure rate alarm system for aircraft |
| US4980684A (en) * | 1983-06-10 | 1990-12-25 | Sundstrand Data Controls, Inc. | Warning system for tactical rotary wing aircraft |
| US5220322A (en) * | 1984-07-18 | 1993-06-15 | Sundstrand Corporation | Ground proximity warning system for use with aircraft having egraded performance |
| IL75701A0 (en) * | 1984-07-18 | 1985-11-29 | Sundstrand Data Control | Ground proximity warning system for aircraft |
| CA1243119A (en) * | 1985-02-22 | 1988-10-11 | Michael M. Grove | Aircraft terrain warning system with configuration modified warning and improved mode switching |
| CA1243118A (en) * | 1985-02-22 | 1988-10-11 | Michael M. Grove | Aircraft terrain closure warning system with descent rate based envelope modification |
| DE3786803D1 (de) * | 1987-11-17 | 1993-09-02 | Litef Gmbh | Verfahren zur erhoehung der fehlererkennung bei der geschwindigkeitsmessung von fluggeraeten mittels doppler-radar. |
| US5900827A (en) * | 1988-06-07 | 1999-05-04 | The Boeing Company | Flight crew response monitor |
| US5136512A (en) * | 1988-06-26 | 1992-08-04 | Cubic Defense Systems, Inc. | Ground collision avoidance system |
| US5260702A (en) * | 1989-12-27 | 1993-11-09 | Thompson Keith P | Aircraft information system |
| US5666110A (en) * | 1995-03-09 | 1997-09-09 | Paterson; Noel S. | Helicopter enhanced descent after take-off warning for GPWS |
| US6606034B1 (en) | 1995-07-31 | 2003-08-12 | Honeywell International Inc. | Terrain awareness system |
| US6138060A (en) * | 1995-07-31 | 2000-10-24 | Alliedsignal 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 |
| US6292721B1 (en) | 1995-07-31 | 2001-09-18 | Allied Signal Inc. | Premature descent into terrain visual awareness enhancement to EGPWS |
| US6092009A (en) | 1995-07-31 | 2000-07-18 | Alliedsignal | Aircraft terrain information system |
| US5781126A (en) * | 1996-07-29 | 1998-07-14 | Alliedsignal Inc. | Ground proximity warning system and methods for rotary wing aircraft |
| US6043759A (en) * | 1996-07-29 | 2000-03-28 | Alliedsignal | Air-ground logic system and method for rotary wing aircraft |
| WO2000023967A1 (en) | 1998-10-16 | 2000-04-27 | Universal Avionics Systems Corporation | Flight plan intent alert system and method |
| DE60030413T2 (de) | 1999-02-01 | 2007-09-13 | Honeywell International Inc. | Verfahren, Vorrichtung und Computerprogrammprodukte zum Bestimmen einer korrigierten Entfernung zwischen einem Flugzeug und einer gewählten Landebahn |
| EP1151429B1 (en) | 1999-02-01 | 2004-04-07 | Honeywell International Inc. | System for generating altitudes above a selected runway |
| US6484071B1 (en) | 1999-02-01 | 2002-11-19 | Honeywell International, Inc. | Ground proximity warning system, method and computer program product for controllably altering the base width of an alert envelope |
| EP1151244B1 (en) | 1999-02-01 | 2009-03-18 | Honeywell International Inc. | Ground proximity warning system |
| 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 |
| US6785594B1 (en) | 1999-03-25 | 2004-08-31 | Honeywell International Inc. | Ground proximity warning system and method having a reduced set of input parameters |
| US6469664B1 (en) | 1999-10-05 | 2002-10-22 | Honeywell International Inc. | Method, apparatus, and computer program products for alerting surface vessels to hazardous conditions |
| US6734808B1 (en) | 1999-10-05 | 2004-05-11 | Honeywell International Inc. | Method, apparatus and computer program products for alerting submersible vessels to hazardous conditions |
| US6583733B2 (en) | 2000-05-26 | 2003-06-24 | Honeywell International Inc. | Apparatus, method and computer program product for helicopter ground proximity warning system |
| US6833797B2 (en) | 2000-05-26 | 2004-12-21 | Honeywell International Inc. | Method, apparatus and computer program product for displaying terrain in rotary wing aircraft |
| AU2001281355A1 (en) * | 2000-07-27 | 2002-02-13 | Innovative Solutions And Support Inc. | Method and system for high precision altitude measurement over hostile terrain |
| WO2002023125A1 (en) | 2000-09-14 | 2002-03-21 | Honeywell International Inc. | Method, apparatus and computer program product for helicopter tail strike warning |
| WO2003008908A1 (en) * | 2001-07-17 | 2003-01-30 | Honeywell International Inc. | Pitch angle alerting device for ground proximity warning system (egpws) |
| US6631315B1 (en) * | 2002-03-14 | 2003-10-07 | Honeywell Inc. | Aircraft signal definition for flight safety system monitoring system |
| FR2840073B1 (fr) * | 2002-05-23 | 2004-07-16 | Eurocopter France | Procede et dispositif pour estimer au moins la vitesse verticale d'un aeronef, en particulier d'un aeronef a voilure tournante |
| US7328114B2 (en) * | 2005-12-09 | 2008-02-05 | General Electric Company | Methods and systems for measuring a rate of change of frequency |
| US7633430B1 (en) * | 2007-09-14 | 2009-12-15 | Rockwell Collins, Inc. | Terrain awareness system with false alert suppression |
| US20090201287A1 (en) * | 2008-02-07 | 2009-08-13 | Honeywell International Inc. | System and method of adaptively filtering parametric data for display |
| FR2956512B1 (fr) * | 2010-02-16 | 2012-03-09 | Airbus Operations Sas | Procede et dispositif de protection automatique d'un aeronef contre un taux de descente excessif. |
| FR2964466B1 (fr) | 2010-09-06 | 2012-10-12 | Airbus Operations Sas | Procede et dispositif de detection automatique d'une valeur de hauteur erronee fournie par un radioaltimetre monte sur un aeronef. |
| US8532848B2 (en) * | 2010-10-19 | 2013-09-10 | Honeywell International Inc. | Systems and methods for alerting potential tailstrike during landing |
| CN105203075B (zh) * | 2015-09-15 | 2017-07-28 | 北京安达维尔航空设备有限公司 | 无线电高度表数据融合测高系统以及测高方法 |
| CN108701257B (zh) | 2016-08-22 | 2023-01-06 | 甲骨文国际公司 | 用于实时可视模拟内的动态、增量推荐的系统和方法 |
| US10816999B2 (en) * | 2018-06-01 | 2020-10-27 | Textron Innovations Inc. | System and method for controlling rotorcraft |
| FR3135253B1 (fr) | 2022-05-09 | 2024-08-16 | Schulz Jean Michel | Dispositif de stockage et de distribution d’hydrogène pour aéronef. |
| FR3136260A1 (fr) | 2022-06-01 | 2023-12-08 | Jean Michel SCHULZ | Générateur cryogénique d’hydrogène gazeux pressurisé - surpresseur cryogénique |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3055214A (en) * | 1956-04-12 | 1962-09-25 | Honeywell Regulator Co | Aircraft instruments |
| US3140483A (en) * | 1959-04-03 | 1964-07-07 | Stephen J Sikora | Barometric-radar altitude control system |
| US3077557A (en) * | 1960-09-30 | 1963-02-12 | Sperry Rand Corp | Flight path computer |
-
1970
- 1970-08-11 US US00062861A patent/US3715718A/en not_active Expired - Lifetime
-
1971
- 1971-07-27 CA CA119,230A patent/CA959577A/en not_active Expired
- 1971-08-02 AU AU31914/71A patent/AU465701B2/en not_active Expired
- 1971-08-04 DE DE2139075A patent/DE2139075C2/de not_active Expired
- 1971-08-10 SE SE7110192A patent/SE379584B/xx unknown
- 1971-08-10 FR FR7129254A patent/FR2102182B1/fr not_active Expired
- 1971-08-11 GB GB3764471A patent/GB1352531A/en not_active Expired
- 1971-08-11 JP JP6036571A patent/JPS5427640B1/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| US3715718A (en) | 1973-02-06 |
| GB1352531A (en) | 1974-05-08 |
| SE379584B (https=) | 1975-10-13 |
| DE2139075A1 (de) | 1972-02-17 |
| AU3191471A (en) | 1973-02-08 |
| FR2102182B1 (https=) | 1977-01-21 |
| FR2102182A1 (https=) | 1972-04-07 |
| JPS5427640B1 (https=) | 1979-09-11 |
| AU465701B2 (en) | 1975-10-02 |
| CA959577A (en) | 1974-12-17 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| OD | Request for examination | ||
| D2 | Grant after examination | ||
| 8328 | Change in the person/name/address of the agent |
Free format text: BEETZ SEN., R., DIPL.-ING. BEETZ JUN., R., DIPL.-ING. DR.-ING. TIMPE, W., DR.-ING. SIEGFRIED, J., DIPL.-ING. SCHMITT-FUMIAN, W., PRIVATDOZENT, DIPL.-CHEM. DR.RER.NAT., PAT.-ANW., 8000 MUENCHEN |
|
| 8339 | Ceased/non-payment of the annual fee |