FR1267275A - Dispositif indicateur d'atterrissage à la verticale - Google Patents
Dispositif indicateur d'atterrissage à la verticaleInfo
- Publication number
- FR1267275A FR1267275A FR829474A FR829474A FR1267275A FR 1267275 A FR1267275 A FR 1267275A FR 829474 A FR829474 A FR 829474A FR 829474 A FR829474 A FR 829474A FR 1267275 A FR1267275 A FR 1267275A
- Authority
- FR
- France
- Prior art keywords
- indicator device
- vertical landing
- landing indicator
- vertical
- 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
- G06—COMPUTING; CALCULATING OR COUNTING
- G06G—ANALOGUE COMPUTERS
- G06G7/00—Devices in which the computing operation is performed by varying electric or magnetic quantities
- G06G7/48—Analogue computers for specific processes, systems or devices, e.g. simulators
- G06G7/78—Analogue computers for specific processes, systems or devices, e.g. simulators for direction-finding, locating, distance or velocity measuring, or navigation systems
-
- 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
- G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
-
- 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)
- Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Computer Hardware Design (AREA)
- Theoretical Computer Science (AREA)
- Mathematical Physics (AREA)
- Traffic Control Systems (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR829474A FR1267275A (fr) | 1960-06-09 | 1960-06-09 | Dispositif indicateur d'atterrissage à la verticale |
US113800A US3152248A (en) | 1960-06-09 | 1961-05-31 | Indicator device for vertical landings |
GB20532/61A GB965276A (en) | 1960-06-09 | 1961-06-07 | Indicator device for vertical-landing aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR829474A FR1267275A (fr) | 1960-06-09 | 1960-06-09 | Dispositif indicateur d'atterrissage à la verticale |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1267275A true FR1267275A (fr) | 1961-07-21 |
Family
ID=8733045
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR829474A Expired FR1267275A (fr) | 1960-06-09 | 1960-06-09 | Dispositif indicateur d'atterrissage à la verticale |
Country Status (2)
Country | Link |
---|---|
US (1) | US3152248A (fr) |
FR (1) | FR1267275A (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0025614A1 (fr) * | 1979-07-23 | 1981-03-25 | The Boeing Company | Méthode et appareillage pour déterminer continûment un intervalle de temps au cours duquel une action doit être entreprise |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1506111A1 (de) * | 1966-04-28 | 1969-10-09 | Teldix Gmbh | Geraet zur Anzeige von Landeinformationen fuer VTOL Flugzeuge |
US3505504A (en) * | 1967-12-21 | 1970-04-07 | Frank J Walker | Altitude pacer system |
US3537323A (en) * | 1968-09-11 | 1970-11-03 | Aerostructures Inc | Hover-altitude performance indicator for a helicopter |
US3774017A (en) * | 1971-10-21 | 1973-11-20 | Honeywell Inc | Apparatus and method for achieving optimum performance of an airplane |
US10836487B2 (en) * | 2018-11-26 | 2020-11-17 | Category, LLC | System for unassisted sky diving |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2246163A (en) * | 1939-01-04 | 1941-06-17 | Gen Electric | Battery charging |
US2930549A (en) * | 1954-08-11 | 1960-03-29 | Snecma | Control device for vertical landing |
US2911143A (en) * | 1954-11-17 | 1959-11-03 | Secr Defence Brit | Means for polar coordinate navigation |
US2845649A (en) * | 1955-08-23 | 1958-08-05 | Robert W Hutson | Brush |
US2878775A (en) * | 1956-03-30 | 1959-03-24 | Burroughs Corp | Reset mechanism for accelerometers |
US2992558A (en) * | 1957-04-29 | 1961-07-18 | Sperry Rand Corp | Flight range and endurance data indicator |
-
1960
- 1960-06-09 FR FR829474A patent/FR1267275A/fr not_active Expired
-
1961
- 1961-05-31 US US113800A patent/US3152248A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0025614A1 (fr) * | 1979-07-23 | 1981-03-25 | The Boeing Company | Méthode et appareillage pour déterminer continûment un intervalle de temps au cours duquel une action doit être entreprise |
Also Published As
Publication number | Publication date |
---|---|
US3152248A (en) | 1964-10-06 |
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