FR2393360A1 - DIGITAL IN-FLIGHT GUIDANCE SYSTEM FOR AIRCRAFT - Google Patents
DIGITAL IN-FLIGHT GUIDANCE SYSTEM FOR AIRCRAFTInfo
- Publication number
- FR2393360A1 FR2393360A1 FR7813630A FR7813630A FR2393360A1 FR 2393360 A1 FR2393360 A1 FR 2393360A1 FR 7813630 A FR7813630 A FR 7813630A FR 7813630 A FR7813630 A FR 7813630A FR 2393360 A1 FR2393360 A1 FR 2393360A1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- digital
- guidance system
- flight guidance
- during
- 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.)
- Granted
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
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls
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)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Safety Devices In Control Systems (AREA)
- Control By Computers (AREA)
Abstract
Système numérique de guidage en vol pour aéronef. Système comprenant une paire de processeurs; chacun ayant une mémoire associée et utilisant un dispositif commun entrée/sortie, et destiné à procurer le guidage surveillé d'un aéronef durant les modes de croisière et durant des manoeuvres critiqués, comme l'atterrissage; chaque processeur effectue certaines des fonctions de l'autre, mais d'une manière différenteDigital in-flight guidance system for aircraft. System comprising a pair of processors; each having an associated memory and using a common input / output device, and intended to provide monitored guidance of an aircraft during cruise modes and during criticized maneuvers, such as landing; each processor performs some of the functions of the other, but in a different way
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US80268577A | 1977-06-02 | 1977-06-02 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2393360A1 true FR2393360A1 (en) | 1978-12-29 |
FR2393360B1 FR2393360B1 (en) | 1982-12-17 |
Family
ID=25184427
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7813630A Granted FR2393360A1 (en) | 1977-06-02 | 1978-05-09 | DIGITAL IN-FLIGHT GUIDANCE SYSTEM FOR AIRCRAFT |
Country Status (4)
Country | Link |
---|---|
JP (1) | JPS543799A (en) |
DE (1) | DE2824279A1 (en) |
FR (1) | FR2393360A1 (en) |
GB (1) | GB1587792A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5671103A (en) * | 1979-11-15 | 1981-06-13 | Toshiba Corp | Control device of power plant |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2104778A1 (en) * | 1970-07-09 | 1972-04-21 | United Kingdom Government | |
US3688099A (en) * | 1971-04-28 | 1972-08-29 | Lear Siegler Inc | Automatic control system with a digital computer |
FR2245020A1 (en) * | 1973-09-24 | 1975-04-18 | Smiths Industries Ltd |
-
1978
- 1978-05-03 GB GB17528/78A patent/GB1587792A/en not_active Expired
- 1978-05-09 FR FR7813630A patent/FR2393360A1/en active Granted
- 1978-05-31 JP JP6564678A patent/JPS543799A/en active Granted
- 1978-06-02 DE DE19782824279 patent/DE2824279A1/en active Granted
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2104778A1 (en) * | 1970-07-09 | 1972-04-21 | United Kingdom Government | |
US3688099A (en) * | 1971-04-28 | 1972-08-29 | Lear Siegler Inc | Automatic control system with a digital computer |
FR2245020A1 (en) * | 1973-09-24 | 1975-04-18 | Smiths Industries Ltd |
Also Published As
Publication number | Publication date |
---|---|
DE2824279C2 (en) | 1989-04-20 |
FR2393360B1 (en) | 1982-12-17 |
DE2824279A1 (en) | 1978-12-14 |
JPS543799A (en) | 1979-01-12 |
JPS6365961B2 (en) | 1988-12-19 |
GB1587792A (en) | 1981-04-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |