SE8100891L - Markvarnande anordning for flygplan - Google Patents
Markvarnande anordning for flygplanInfo
- Publication number
- SE8100891L SE8100891L SE8100891A SE8100891A SE8100891L SE 8100891 L SE8100891 L SE 8100891L SE 8100891 A SE8100891 A SE 8100891A SE 8100891 A SE8100891 A SE 8100891A SE 8100891 L SE8100891 L SE 8100891L
- Authority
- SE
- Sweden
- Prior art keywords
- signal
- aircraft
- slide
- warning
- ground
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/20—Arrangements for acquiring, generating, sharing or displaying traffic information
- G08G5/21—Arrangements for acquiring, generating, sharing or displaying traffic information located onboard the aircraft
-
- 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
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft
- G08G5/50—Navigation or guidance aids
- G08G5/54—Navigation or guidance aids for approach or landing
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Traffic Control Systems (AREA)
- Radar Systems Or Details Thereof (AREA)
- Emergency Alarm Devices (AREA)
- Navigation (AREA)
- Alarm Systems (AREA)
Claims (1)
1. PATENTKRAV Varningsinstrument inrgttat att gbra photon i en flygfarkost unpmgrksam pS ett tillstAnd an ej Onskad ngrhet till marken Yid en flygplats, som gr utrustad med en sandare fbr glidbaneradiostrAle, silken strAle innefattar giltig och synbarligen giltig stignings- och sjunkningsinformation, varvid instrumentet innefattar en i flygfarkosten fdrefintlig mottagare (37), som gr pAyerkbar i beroende an glidbaneradiostrAlen for alstring an en signal (6/5) som representerar riktningen och stcrleken has vinkelayvikelse fbr flygfarkostens lgge Over eller under den medelst glidbaneradiostrilen bestgmda glidbanan, en i beroende as signalen frAn motLagaren (37) pAyerkbar detektor (87) fdr detektering an en, en avvikelse Under glidbanan indiketande avvikelsesignal, som.representerar ett tillstand under glidbanan byerstigande ett faststgllt yard°, varvid detektorn Or anordnad att alstra en, en yarning on att flygfarkosten befinner sig under glidbanan initierande signal, ocb en hbjdsignalkglla (26) fbr alstring on en signal, son representerar flygfarkostens hbjd, en i beroende as heddsignalkallan (26)-Overkbar konditioneringskrets (88-9l) inrattad att son funktion at hdjden yariera det faststallda vgrdet fbr tillstAndet under glidbanan fbr att konditionera detektorn (87) till att alstra den, en yarning on att flygfarkosten befinner sig under glidbanan initierande signalen, en kretsanordning (86) inrattad att, nar flygfarkosten befinner sig under en fbrutbestemdinhibera den en VP' 'ng no att flygfarkosten befinner sig under glidbanan initia signalen, OCtretsanordning (52) som Sr kopplad for att vara pAverkbar i beroende ay den, en Yarning am att flygfarkosten befinner sig under glidbanan initierande signalen i och fbr att aktivera en piloty ningsanordning (54), k a n ne t e c km a t an att en summeringsanordning (82) or kopplad fbr summering an en signal, son representerar en funktion av flygfarkost( hbjd Over marken, and en signal, sun representerar en funktion ay Andringshastighl tins flygfarkostens hdjd Over marken, att en detektor (83) gr kopplad fbr att vara pAverkbar i beroende an summatignalen i och fbr detektering an en Andringshastighl hos hdjden Over marken, son bverskrider ett fbrutbestgmt ygrde for flygfarkostens hbjd Over marken, fbr att alstra en varningsstyrsignal for gndringshastigheten no marken, att en ELLER-grind (52) Sr kopplad med en ingAng pAyerkbar i beroende av ngmnda yarningsstyrsignal och en annan ingAng pAverkbar i beroende as glidbane- varningssignalen i och for alstring av varningsinitieringsutsignalen ngr endera varningssignalen opptrgder, och att pilotvarningsanordningen (54) gr ofiverkbar i beroende an en varningsinitieringsuttignal frAn ELLER-grinden. 66167 # 4m/min -145 m 60 GU hRt' 21Q 390 mimir. 7/ ÔI10 miTin 74 Test i lurten 77 'TB Varningsenhat -ei 3 —ELI— C 54. . Under 0/S • so 1 Start Marisch egativ stigningshastighet 7-111:11 I/I/FD 64Mark:7" 4. FD Rarkteot.GooK GX 63 240 is/min
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/480,727 US3946358A (en) | 1974-06-19 | 1974-06-19 | Aircraft ground proximity warning instrument |
Publications (2)
Publication Number | Publication Date |
---|---|
SE8100891L true SE8100891L (sv) | 1981-02-09 |
SE449598B SE449598B (sv) | 1987-05-11 |
Family
ID=23909109
Family Applications (6)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE7506677A SE418720B (sv) | 1974-06-19 | 1975-06-11 | Varningsinstrument for flygfarkoster |
SE7808631A SE424624B (sv) | 1974-06-19 | 1978-08-15 | Varningsinstrument i flygfarkost |
SE8100889A SE422715B (sv) | 1974-06-19 | 1981-02-09 | Varningsinstrument i en flygfarkost |
SE8100891A SE449598B (sv) | 1974-06-19 | 1981-02-09 | Markvarnande instrument for flygplan |
SE8100892A SE449599B (sv) | 1974-06-19 | 1981-02-09 | Markvarnande instrument for flygplan |
SE8100890A SE422671B (sv) | 1974-06-19 | 1981-02-09 | Varningsinstrument i flygfarkost |
Family Applications Before (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE7506677A SE418720B (sv) | 1974-06-19 | 1975-06-11 | Varningsinstrument for flygfarkoster |
SE7808631A SE424624B (sv) | 1974-06-19 | 1978-08-15 | Varningsinstrument i flygfarkost |
SE8100889A SE422715B (sv) | 1974-06-19 | 1981-02-09 | Varningsinstrument i en flygfarkost |
Family Applications After (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8100892A SE449599B (sv) | 1974-06-19 | 1981-02-09 | Markvarnande instrument for flygplan |
SE8100890A SE422671B (sv) | 1974-06-19 | 1981-02-09 | Varningsinstrument i flygfarkost |
Country Status (9)
Country | Link |
---|---|
US (1) | US3946358A (sv) |
JP (2) | JPS5934560B2 (sv) |
AU (2) | AU499009B2 (sv) |
CA (1) | CA1043005A (sv) |
DE (2) | DE2559952C3 (sv) |
FR (2) | FR2309939A1 (sv) |
GB (2) | GB1488744A (sv) |
IT (1) | IT1040627B (sv) |
SE (6) | SE418720B (sv) |
Families Citing this family (64)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3946358A (en) * | 1974-06-19 | 1976-03-23 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning instrument |
JPS5174333A (en) * | 1974-12-23 | 1976-06-28 | Honda Motor Co Ltd | Sharyoni okeru keihosochi |
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 |
US4016565A (en) * | 1975-09-15 | 1977-04-05 | Rockwell International Corporation | Aircraft ground closure rate filtering method and means |
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 |
US4060793A (en) * | 1976-07-19 | 1977-11-29 | Sundstrand Data Control, Inc. | Excessive sink rate warning system for aircraft |
US4030065A (en) * | 1976-07-19 | 1977-06-14 | Sundstrand Corporation | Terrain clearance warning system for aircraft |
JPS544172U (sv) * | 1977-06-11 | 1979-01-11 | ||
US4224669A (en) * | 1977-12-22 | 1980-09-23 | The Boeing Company | Minimum safe altitude monitoring, indication and warning system |
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 |
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 |
NZ207653A (en) * | 1983-05-13 | 1987-11-27 | Sundstrand Data Control | Excessive descent rate warning system for aircraft |
US4951047A (en) * | 1983-05-13 | 1990-08-21 | Sunstrand Data Control, Inc. | Negative climb after take-off warning system |
US4639730A (en) * | 1983-05-13 | 1987-01-27 | Sundstrand Data Control, Inc. | Excessive terrain closure warning system |
CA1234417A (en) * | 1983-05-13 | 1988-03-22 | Noel S. Paterson | System for alerting a pilot of a dangerous flight profile during low level maneuvering |
US4939513A (en) * | 1983-05-13 | 1990-07-03 | Sundstrand Data Control, Inc. | System for alerting a pilot of a dangerous flight profile during low level maneuvering |
US5001476A (en) * | 1983-05-13 | 1991-03-19 | Sundstrand Data Control, Inc. | Warning system for tactical aircraft |
US4818992A (en) * | 1983-06-10 | 1989-04-04 | Sundstrand Data Control, Inc. | Excessive altitude loss after take-off warning system for rotary wing aircraft |
US4551723A (en) * | 1983-06-10 | 1985-11-05 | Sundstrand Data Control, Inc. | Excessive descent rate warning system for rotary wing 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 |
US5187478A (en) * | 1985-02-22 | 1993-02-16 | Sundstrand Corporation | Configuration responsive descent rate warning system for aircraft |
CA1243117A (en) * | 1985-02-22 | 1988-10-11 | Michael M. Grove | Altitude loss after take-off warning system utilizing time and altitude |
CA1243118A (en) * | 1985-02-22 | 1988-10-11 | Michael M. Grove | Aircraft terrain closure warning system with descent rate based envelope modification |
CA1243405A (en) * | 1985-02-22 | 1988-10-18 | Michael M. Grove | Configuration responsive descent rate warning system for aircraft |
IL77860A0 (en) * | 1985-02-22 | 1986-09-30 | Sundstrand Data Control | Ground proximity warning system for aircraft |
US4947164A (en) * | 1988-01-21 | 1990-08-07 | Sundstrand Data Control, Inc. | Flight path responsive aircraft wind shear alerting and warning system |
US4916448A (en) * | 1988-02-26 | 1990-04-10 | The United States Of America As Represented By The Secretary Of The Air Force | Low altitude warning system for aircraft |
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 |
US5166682A (en) * | 1991-03-07 | 1992-11-24 | Sundstrand Corporation | Ground proximity warning instrument utilizing glideslope modulation of excessive descent rate envelope |
US5225829A (en) * | 1991-05-09 | 1993-07-06 | Sundstrand Corporation | Independent low airspeed alert |
US5406487A (en) * | 1991-10-11 | 1995-04-11 | Tanis; Peter G. | Aircraft altitude approach control device |
US5666110A (en) * | 1995-03-09 | 1997-09-09 | Paterson; Noel S. | Helicopter enhanced descent after take-off warning for GPWS |
US5745053A (en) * | 1995-12-08 | 1998-04-28 | Fleming, Iii; Hoyt A. | Landing gear warning apparatus and method for pilots approaching a runway with retracted landing gear |
US6043758A (en) * | 1996-02-12 | 2000-03-28 | Alliedsignal Inc. | Terrain warning system |
US6008742A (en) * | 1997-05-21 | 1999-12-28 | Groves; Duane | Aircraft landing gear warning system |
JP4551562B2 (ja) | 1998-10-16 | 2010-09-29 | ユニバーサル エイビーアニクス システムズ コーポレイション | 飛行計画目的警報システムおよび方法 |
US6421603B1 (en) | 1999-08-11 | 2002-07-16 | Honeywell International Inc. | Hazard detection for a travel plan |
WO2002059547A2 (en) * | 2001-01-23 | 2002-08-01 | Honeywell International Inc. | Egpws cutoff altitude for helicopters |
EP1407226A1 (en) * | 2001-07-17 | 2004-04-14 | Honeywell International Inc. | Pitch angle alerting device for ground proximity warning systems (gpws) |
GB2387912A (en) * | 2002-04-26 | 2003-10-29 | Messier Dowty Inc | Monitoring parameters in structural components |
US7633410B2 (en) * | 2004-02-19 | 2009-12-15 | Honeywell International Inc. | Wireless assisted recovery systems and methods |
US7274309B2 (en) * | 2005-03-29 | 2007-09-25 | Nance C Kirk | Aircraft landing gear initial touch-down velocity monitor |
US7274310B1 (en) | 2005-03-29 | 2007-09-25 | Nance C Kirk | Aircraft landing gear kinetic energy monitor |
US7209053B2 (en) * | 2005-04-06 | 2007-04-24 | Honeywell International Inc. | System and method for displaying validity of airport visual approach slope indicators |
US7633430B1 (en) * | 2007-09-14 | 2009-12-15 | Rockwell Collins, Inc. | Terrain awareness system with false alert suppression |
US8042765B1 (en) | 2008-05-20 | 2011-10-25 | Nance C Kirk | Aircraft landing gear compression rate monitor |
FR2938683B1 (fr) * | 2008-11-14 | 2012-06-15 | Airbus France | Procede et systeme d'evitement de terrain pour un aeronef |
RU2449923C1 (ru) * | 2010-11-15 | 2012-05-10 | Открытое акционерное общество Московский научно-производственный комплекс "Авионика" имени О.В. Успенского (ОАО МНПК "Авионика") | Система автоматического управления самолетом при заходе на посадку |
RU2449922C1 (ru) * | 2010-11-15 | 2012-05-10 | Открытое акционерное общество Московский научно-производственный комплекс "Авионика" имени О.В. Успенского (ОАО МНПК "Авионика") | Способ автоматического управления самолетом при заходе на посадку |
US8554396B2 (en) * | 2012-01-03 | 2013-10-08 | Honeywell International Inc. | Systems and methods for issuing a hard landing warning and providing maintenance advisories for hard landing incidents |
US9284047B2 (en) * | 2013-08-02 | 2016-03-15 | Goodrich Corporation | Routings for articulated landing gear |
US10089634B2 (en) | 2015-10-27 | 2018-10-02 | C Kirk Nance | Method to recover non-recognized errors in aircraft weight determinations to increase weight and center of gravity limitations for regulated aircraft |
US9751636B2 (en) | 2015-12-15 | 2017-09-05 | International Business Machines Corporation | Dynamic detection of landing gear deployment |
FR3072490B1 (fr) * | 2017-10-17 | 2019-11-08 | Airbus Operations (S.A.S.) | Systeme et procede d'aide a l'atterrissage d'un aeronef |
US20240411323A1 (en) * | 2023-06-08 | 2024-12-12 | Honeywell International Inc. | Avionic System and Method for Selectively Preventing and Enhanced Ground Proximity Warning System Alert Mode from Generating an Alert |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB866125A (en) | 1958-07-16 | 1961-04-26 | Secr Aviation | Improvements in or relating to warning devices for aircraft |
US3052427A (en) * | 1960-07-08 | 1962-09-04 | Sperry Rand Corp | Flare-out system for aircraft |
US3169730A (en) * | 1962-11-01 | 1965-02-16 | Sperry Rand Corp | Flight control system |
US3355733A (en) * | 1964-10-19 | 1967-11-28 | Bell Aerospace Corp | Designated area instrument landing system |
US3327973A (en) * | 1965-06-14 | 1967-06-27 | Lear Siegler Inc | Automatic landing pitch axis control system for aircraft |
GB1178842A (en) * | 1966-01-29 | 1970-01-21 | Elliott Brothers London Ltd | Improvements in and relating to the Control of Aircraft |
US3743221A (en) * | 1970-04-09 | 1973-07-03 | Lear Siegler Inc | Aircraft flight control apparatus |
US3652835A (en) * | 1970-05-14 | 1972-03-28 | Sperry Rand Corp | Aircraft glide slope coupler system |
US3715718A (en) * | 1970-08-11 | 1973-02-06 | Sundstrand Data Control | Ground proximity warning system utilizing radio and barometric altimeter combination |
US3658280A (en) * | 1970-10-29 | 1972-04-25 | Mc Donnell Douglas Corp | Altitude and glide slope track controller |
US3757338A (en) * | 1971-02-05 | 1973-09-04 | Bendix Corp | Glide slope lock-out network |
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 |
US3860800A (en) * | 1972-06-19 | 1975-01-14 | Boeing Co | Automatic pitch axis control system for aircraft |
US3946358A (en) | 1974-06-19 | 1976-03-23 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning instrument |
-
1974
- 1974-06-19 US US05/480,727 patent/US3946358A/en not_active Expired - Lifetime
-
1975
- 1975-06-11 SE SE7506677A patent/SE418720B/sv not_active IP Right Cessation
- 1975-06-13 AU AU82128/75A patent/AU499009B2/en not_active Expired
- 1975-06-17 CA CA229,500A patent/CA1043005A/en not_active Expired
- 1975-06-18 DE DE2559952A patent/DE2559952C3/de not_active Expired
- 1975-06-18 FR FR7519138A patent/FR2309939A1/fr active Granted
- 1975-06-18 IT IT50109/75A patent/IT1040627B/it active
- 1975-06-18 DE DE2527056A patent/DE2527056C3/de not_active Expired
- 1975-06-19 GB GB26061/75A patent/GB1488744A/en not_active Expired
- 1975-06-19 GB GB8270/76A patent/GB1488745A/en not_active Expired
- 1975-06-19 JP JP50073848A patent/JPS5934560B2/ja not_active Expired
- 1975-12-31 FR FR7540307A patent/FR2289980A1/fr active Granted
-
1978
- 1978-08-15 SE SE7808631A patent/SE424624B/sv not_active IP Right Cessation
- 1978-12-18 AU AU42665/78A patent/AU511815B2/en not_active Expired
-
1981
- 1981-02-09 SE SE8100889A patent/SE422715B/sv not_active IP Right Cessation
- 1981-02-09 SE SE8100891A patent/SE449598B/sv not_active IP Right Cessation
- 1981-02-09 SE SE8100892A patent/SE449599B/sv not_active IP Right Cessation
- 1981-02-09 SE SE8100890A patent/SE422671B/sv not_active IP Right Cessation
-
1982
- 1982-07-31 JP JP57134616A patent/JPS5861100A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
SE449599B (sv) | 1987-05-11 |
SE8100890L (sv) | 1981-02-09 |
GB1488744A (en) | 1977-10-12 |
SE422715B (sv) | 1982-03-22 |
GB1488745A (en) | 1977-10-12 |
JPS5861100A (ja) | 1983-04-11 |
DE2527056A1 (de) | 1976-01-02 |
SE7808631L (sv) | 1978-08-15 |
JPS5114699A (en) | 1976-02-05 |
DE2527056C3 (de) | 1979-10-11 |
SE418720B (sv) | 1981-06-22 |
AU499009B2 (en) | 1979-04-05 |
JPS5934560B2 (ja) | 1984-08-23 |
SE422671B (sv) | 1982-03-22 |
DE2527056B2 (de) | 1979-02-15 |
FR2289980B1 (sv) | 1979-05-04 |
SE424624B (sv) | 1982-08-02 |
FR2309939B1 (sv) | 1980-07-25 |
AU511815B2 (en) | 1980-09-04 |
SE8100889L (sv) | 1981-02-09 |
CA1043005A (en) | 1978-11-21 |
US3946358A (en) | 1976-03-23 |
SE8100892L (sv) | 1981-02-09 |
DE2559952C3 (de) | 1981-07-02 |
IT1040627B (it) | 1979-12-20 |
JPS6253051B2 (sv) | 1987-11-09 |
FR2309939A1 (fr) | 1976-11-26 |
SE449598B (sv) | 1987-05-11 |
AU8212875A (en) | 1976-12-16 |
FR2289980A1 (fr) | 1976-05-28 |
SE7506677L (sv) | 1975-12-22 |
DE2559952B1 (de) | 1980-11-20 |
AU4266578A (en) | 1979-04-05 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
SE8100891L (sv) | Markvarnande anordning for flygplan | |
US3944968A (en) | Aircraft ground proximity warning system having speed versus altitude compensation | |
US3947809A (en) | Below glide slope advisory warning system for aircraft | |
EP3327534B1 (en) | Flight control system with low-frequency anomaly detection of ils localizer data and associated method | |
JPS6047966B2 (ja) | 航空機の異常降下速度の警報発生装置 | |
CA1205167A (en) | Ground proximity warning system with time and altitude based mode switching | |
US3752967A (en) | Ascent and descent slope tracker system | |
US3522729A (en) | Airspeed command system | |
US5187478A (en) | Configuration responsive descent rate warning system for aircraft | |
JP5312048B2 (ja) | 航空機周囲の気流の全体の温度を決定する方法 | |
US3681580A (en) | Rotation,climbout,and go-around control system | |
US5038141A (en) | Configuration responsive descent rate warning system for aircraft | |
US4042197A (en) | Automatic controls for airplane take-off and landing modes | |
US3988713A (en) | Aircraft ground proximity warning instrument | |
EP0020550A1 (en) | Improved method and apparatus for detecting clear air turbulences | |
US3496769A (en) | Descent-approach system for aircraft | |
US4281383A (en) | Process and system for the rapid detection of a wind gradient | |
US4937571A (en) | System for elaborating an alarm signal on board an aircraft in the event of a mini-tornado | |
US3709033A (en) | Velocity monitor for aircraft | |
CN111026159A (zh) | 一种直升机飞控系统bc反航道导航功能的实现方法 | |
FI74247B (fi) | Varningssystem foer flygplan, som landar med landningsstaellet uppfaellt. | |
US2646564A (en) | Radio navigation system | |
US3478310A (en) | Aircraft command altitude guidance apparatus | |
US3682417A (en) | Engagement of altitude hold mode in aircraft flight control system | |
US2939652A (en) | Aircraft landing system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |
Ref document number: 8100891-4 Effective date: 19890725 Format of ref document f/p: F |