FR2325022A1 - Procede et appareil de controle de la trajectoire de vol d'un avion - Google Patents
Procede et appareil de controle de la trajectoire de vol d'un avionInfo
- Publication number
- FR2325022A1 FR2325022A1 FR6911680A FR6911680A FR2325022A1 FR 2325022 A1 FR2325022 A1 FR 2325022A1 FR 6911680 A FR6911680 A FR 6911680A FR 6911680 A FR6911680 A FR 6911680A FR 2325022 A1 FR2325022 A1 FR 2325022A1
- Authority
- FR
- France
- Prior art keywords
- pilot
- head
- aircraft
- terrain
- information display
- 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.)
- Withdrawn
Links
- 239000012141 concentrate Substances 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C23/00—Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
- G01C23/005—Flight directors
-
- 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
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
- G01S7/04—Display arrangements
- G01S7/06—Cathode-ray tube displays or other two dimensional or three-dimensional displays
- G01S7/20—Stereoscopic displays; Three-dimensional displays; Pseudo-three-dimensional displays
-
- 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
- G05D1/0646—Rate of change of altitude or depth specially adapted for aircraft to follow the profile of undulating ground
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Computer Networks & Wireless Communication (AREA)
- Automation & Control Theory (AREA)
- Radar Systems Or Details Thereof (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR6911680A FR2325022A1 (fr) | 1969-05-02 | 1969-05-02 | Procede et appareil de controle de la trajectoire de vol d'un avion |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR6911680A FR2325022A1 (fr) | 1969-05-02 | 1969-05-02 | Procede et appareil de controle de la trajectoire de vol d'un avion |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2325022A1 true FR2325022A1 (fr) | 1977-04-15 |
Family
ID=9032447
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR6911680A Withdrawn FR2325022A1 (fr) | 1969-05-02 | 1969-05-02 | Procede et appareil de controle de la trajectoire de vol d'un avion |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2325022A1 (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0273326A2 (fr) * | 1986-12-24 | 1988-07-06 | Deutsche Aerospace AG | Système d'aide à l'atterrissage pour avions comportant leur propre radar de bord |
WO2007010141A2 (fr) * | 2005-07-21 | 2007-01-25 | Airbus | Procede et dispositif de securisation d’un vol automatique a basse altitude d’un aeronef |
FR2914074A1 (fr) * | 2007-03-23 | 2008-09-26 | Thales Sa | Methode de generation de valeurs de consignes servant a asservir un parametre de vol p d'un aeronef equipe d'un pilote automatique. |
-
1969
- 1969-05-02 FR FR6911680A patent/FR2325022A1/fr not_active Withdrawn
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0273326A2 (fr) * | 1986-12-24 | 1988-07-06 | Deutsche Aerospace AG | Système d'aide à l'atterrissage pour avions comportant leur propre radar de bord |
EP0273326A3 (en) * | 1986-12-24 | 1989-09-27 | Licentia Patent-Verwaltungs-Gmbh | Landing-aid system for aircraft having its own on-board radar |
WO2007010141A2 (fr) * | 2005-07-21 | 2007-01-25 | Airbus | Procede et dispositif de securisation d’un vol automatique a basse altitude d’un aeronef |
FR2888955A1 (fr) * | 2005-07-21 | 2007-01-26 | Airbus Sas | Procede et dispositif de securisation d'un vol automatique a basse altitude d'un aeronef |
WO2007010141A3 (fr) * | 2005-07-21 | 2007-04-12 | Airbus | Procede et dispositif de securisation d’un vol automatique a basse altitude d’un aeronef |
CN101228490B (zh) * | 2005-07-21 | 2010-05-19 | 空中巴士公司 | 用于保障飞行器的低空自动飞行的方法、设备和飞行器 |
FR2914074A1 (fr) * | 2007-03-23 | 2008-09-26 | Thales Sa | Methode de generation de valeurs de consignes servant a asservir un parametre de vol p d'un aeronef equipe d'un pilote automatique. |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |