FR82158E - Système d'atterrissage d'avions - Google Patents
Système d'atterrissage d'avionsInfo
- Publication number
- FR82158E FR82158E FR902352A FR902352A FR82158E FR 82158 E FR82158 E FR 82158E FR 902352 A FR902352 A FR 902352A FR 902352 A FR902352 A FR 902352A FR 82158 E FR82158 E FR 82158E
- Authority
- FR
- France
- Prior art keywords
- aircraft landing
- landing system
- aircraft
- landing
- 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
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
- G05D1/04—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
- G05D1/0661—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off
-
- 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
- G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
- G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
- G01S1/022—Means for monitoring or calibrating
-
- 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
- G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
- G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
- G01S1/08—Systems for determining direction or position line
- G01S1/44—Rotating or oscillating beam beacons defining directions in the plane of rotation or oscillation
- G01S1/54—Narrow-beam systems producing at a receiver a pulse-type envelope signal of the carrier wave of the beam, the timing of which is dependent upon the angle between the direction of the receiver from the beacon and a reference direction from the beacon; Overlapping broad beam systems defining a narrow zone and producing at a receiver a pulse-type envelope signal of the carrier wave of the beam, the timing of which is dependent upon the angle between the direction of the receiver from the beacon and a reference direction from the beacon
- G01S1/58—Narrow-beam systems producing at a receiver a pulse-type envelope signal of the carrier wave of the beam, the timing of which is dependent upon the angle between the direction of the receiver from the beacon and a reference direction from the beacon; Overlapping broad beam systems defining a narrow zone and producing at a receiver a pulse-type envelope signal of the carrier wave of the beam, the timing of which is dependent upon the angle between the direction of the receiver from the beacon and a reference direction from the beacon wherein a characteristic of the beam transmitted or of an auxiliary signal is varied in time synchronously with rotation or oscillation of the beam
- G01S1/64—Varying pulse timing, e.g. varying interval between pulses radiated in pairs
-
- 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
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
- G01S5/08—Position of single direction-finder fixed by determining direction of a plurality of spaced sources of known location
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)
- Position Fixing By Use Of Radio Waves (AREA)
- Traffic Control Systems (AREA)
- Radio Relay Systems (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US82546959A | 1959-07-07 | 1959-07-07 | |
US27406A US3191175A (en) | 1959-07-07 | 1960-05-06 | Aircraft landing system |
US123928A US3157877A (en) | 1961-06-28 | 1961-06-28 | Aircraft landing system |
Publications (1)
Publication Number | Publication Date |
---|---|
FR82158E true FR82158E (fr) | 1964-01-04 |
Family
ID=31499166
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR827343A Expired FR1260282A (fr) | 1959-07-07 | 1960-05-16 | Système d'atterrissage d'avions |
FR861024A Expired FR1291865A (fr) | 1959-07-07 | 1961-05-06 | Système de radio navigation aérienne |
FR902352A Expired FR82158E (fr) | 1959-07-07 | 1962-06-28 | Système d'atterrissage d'avions |
Family Applications Before (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR827343A Expired FR1260282A (fr) | 1959-07-07 | 1960-05-16 | Système d'atterrissage d'avions |
FR861024A Expired FR1291865A (fr) | 1959-07-07 | 1961-05-06 | Système de radio navigation aérienne |
Country Status (4)
Country | Link |
---|---|
US (1) | US3191175A (fr) |
DE (1) | DE1287936C2 (fr) |
FR (3) | FR1260282A (fr) |
GB (5) | GB940509A (fr) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1304176A (fr) * | 1961-08-11 | 1962-09-21 | Csf | Système de détermination du site ou de l'azimut d'un mobile |
US3210763A (en) * | 1962-03-19 | 1965-10-05 | Sperry Rand Corp | Flight control system |
FR1347696A (fr) * | 1962-08-23 | 1964-01-04 | Eastman Kodak Co | Nouvelle composition à base de polyester et ses applications |
BE636626A (fr) * | 1962-08-27 | |||
US3309707A (en) * | 1965-03-02 | 1967-03-14 | Cutler Hammer Inc | Guidance computer for aircraft landing system |
US3401389A (en) * | 1967-03-06 | 1968-09-10 | Gen Precision Systems Inc | Tactical landing approach radio system |
US3484167A (en) * | 1967-07-11 | 1969-12-16 | Ibm | Formation flight control system |
US3648231A (en) * | 1969-12-12 | 1972-03-07 | Bendix Corp | Method and means for providing a synthetic real world runway centerline display |
US3601706A (en) * | 1970-03-02 | 1971-08-24 | Cutler Hammer Inc | Pulse interval decoder |
US3757337A (en) * | 1970-09-11 | 1973-09-04 | G Litchford | Aircraft instrument landing system |
USRE28599E (en) * | 1971-01-07 | 1975-10-28 | Tull Aviation Corp | Scanning beam guidance method and system |
US3808558A (en) * | 1971-11-08 | 1974-04-30 | Tull Aviation Corp | Method and apparatus for modulation synthesis |
US3890620A (en) * | 1971-11-08 | 1975-06-17 | Tull Aviation Corp | Method and apparatus for modulation synthesis |
US3793597A (en) * | 1971-11-08 | 1974-02-19 | Tull Aviation Corp | Modulation synthesis method and apparatus |
GB1523887A (en) * | 1974-10-22 | 1978-09-06 | Basov N G | Aircraft take-off and landing system and method for using same |
FR2571862B1 (fr) * | 1984-10-11 | 1988-02-12 | Bloncourt Laurent | Calculateur de navigation pour recepteur a portee optique omnidirectionnel |
US4789864A (en) * | 1987-04-22 | 1988-12-06 | Eaton Corporation | Low elevation guidance system |
US4979669A (en) * | 1989-07-07 | 1990-12-25 | Michael Kerton | Self-closing box |
FR3000831A1 (fr) | 2013-01-09 | 2014-07-11 | Electricite De France | Installation de traitement de dechets radioactifs carbones, notamment de graphite |
KR102665729B1 (ko) | 2015-12-31 | 2024-05-14 | 비아셋, 인크 | 광학 피더 링크들을 사용하는 광대역 위성 통신 시스템 |
CN107745814B (zh) * | 2017-11-15 | 2023-12-22 | 航宇救生装备有限公司 | 一种用于空投系统着陆的主动防翻控制机构 |
CN113093795B (zh) * | 2021-03-30 | 2022-04-22 | 华南理工大学 | 一种水面无人飞船的半自动无线控制方法及装置 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2429630A (en) * | 1943-07-09 | 1947-10-28 | Standard Telephones Cables Ltd | Localizer beacon |
US2449982A (en) * | 1944-06-12 | 1948-09-28 | Standard Telephones Cables Ltd | Radio beacon |
BE480311A (fr) * | 1944-08-18 | |||
US2531918A (en) * | 1946-01-31 | 1950-11-28 | Decca Record Co Ltd | Radio direction indicating device |
US2539905A (en) * | 1946-12-21 | 1951-01-30 | Rca Corp | Air navigation |
US2586810A (en) * | 1947-10-21 | 1952-02-26 | Int Standard Electric Corp | Localizer and glide path system |
US2883662A (en) * | 1950-04-28 | 1959-04-21 | Rodgers George Victor | Pulse operated servomechanism |
US2826378A (en) * | 1950-12-15 | 1958-03-11 | Jr John Norris Childs | Apparatus for radio control of guided missiles |
CH303844A (de) * | 1951-08-30 | 1954-12-15 | Ag Contraves | Verfahren und Vorrichtung zur Fernlenkung eines Flugkörpers. |
US2859440A (en) * | 1956-03-02 | 1958-11-04 | Hughes Aircraft Co | Identification system for airports |
US2864080A (en) * | 1956-03-30 | 1958-12-09 | Rodgers George Victor | Azimuth indicating system |
-
1960
- 1960-04-11 GB GB12809/60A patent/GB940509A/en not_active Expired
- 1960-05-06 US US27406A patent/US3191175A/en not_active Expired - Lifetime
- 1960-05-16 FR FR827343A patent/FR1260282A/fr not_active Expired
-
1961
- 1961-05-01 GB GB15654/61A patent/GB992543A/en not_active Expired
- 1961-05-01 GB GB8933/64A patent/GB992545A/en not_active Expired
- 1961-05-01 GB GB8932/64A patent/GB992544A/en not_active Expired
- 1961-05-06 FR FR861024A patent/FR1291865A/fr not_active Expired
-
1962
- 1962-06-20 GB GB23777/62A patent/GB1014633A/en not_active Expired
- 1962-06-27 DE DE1962C0027319 patent/DE1287936C2/de not_active Expired
- 1962-06-28 FR FR902352A patent/FR82158E/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB992544A (en) | 1965-05-19 |
GB992543A (en) | 1965-05-19 |
US3191175A (en) | 1965-06-22 |
GB992545A (en) | 1965-05-19 |
GB940509A (en) | 1963-10-30 |
DE1287936B (fr) | 1969-01-23 |
GB1014633A (en) | 1965-12-31 |
FR1260282A (fr) | 1961-05-05 |
FR1291865A (fr) | 1962-04-27 |
DE1287936C2 (de) | 1969-09-18 |
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