FR2449592A1 - Avion muni de surfaces de gouverne disposees devant et derriere le centre de gravite - Google Patents
Avion muni de surfaces de gouverne disposees devant et derriere le centre de graviteInfo
- Publication number
- FR2449592A1 FR2449592A1 FR8001343A FR8001343A FR2449592A1 FR 2449592 A1 FR2449592 A1 FR 2449592A1 FR 8001343 A FR8001343 A FR 8001343A FR 8001343 A FR8001343 A FR 8001343A FR 2449592 A1 FR2449592 A1 FR 2449592A1
- Authority
- FR
- France
- Prior art keywords
- governor
- gravity
- behind
- center
- surfaces arranged
- 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
- 230000005484 gravity Effects 0.000 title 1
- 210000000056 organ Anatomy 0.000 abstract 2
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Pressure Circuits (AREA)
- Servomotors (AREA)
- Toys (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19792906889 DE2906889C2 (de) | 1979-02-22 | 1979-02-22 | Flugzeug mit vor und hinter dem Schwerpunkt angeordneten Steuerflächen |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2449592A1 true FR2449592A1 (fr) | 1980-09-19 |
| FR2449592B1 FR2449592B1 (enrdf_load_stackoverflow) | 1984-11-23 |
Family
ID=6063635
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR8001343A Granted FR2449592A1 (fr) | 1979-02-22 | 1980-01-22 | Avion muni de surfaces de gouverne disposees devant et derriere le centre de gravite |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE2906889C2 (enrdf_load_stackoverflow) |
| FR (1) | FR2449592A1 (enrdf_load_stackoverflow) |
| GB (1) | GB2043562B (enrdf_load_stackoverflow) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0680877A1 (fr) * | 1994-05-03 | 1995-11-08 | AEROSPATIALE Société Nationale Industrielle | Avion de transport à empennage avant |
| EP0953504A1 (fr) | 1998-04-29 | 1999-11-03 | Aerospatiale Societe Nationale Industrielle | Aéronef à efforts de voilure diminués |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2112757A (en) * | 1935-03-03 | 1938-03-29 | Billioque Elie Jean Henri | Stabilizing device for aeroplanes |
| FR2405869A1 (fr) * | 1977-10-17 | 1979-05-11 | Onera (Off Nat Aerospatiale) | Procede et installation pour le controle de l'efficacite des surfaces aerodynamiques d'un aeronef |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2355979B2 (de) * | 1973-11-09 | 1976-12-02 | Dornier Gmbh, 7990 Friedrichshafen | Zusaetzliche steuereinrichtung fuer flugzeuge |
-
1979
- 1979-02-22 DE DE19792906889 patent/DE2906889C2/de not_active Expired
-
1980
- 1980-01-22 FR FR8001343A patent/FR2449592A1/fr active Granted
- 1980-02-21 GB GB8005928A patent/GB2043562B/en not_active Expired
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2112757A (en) * | 1935-03-03 | 1938-03-29 | Billioque Elie Jean Henri | Stabilizing device for aeroplanes |
| FR2405869A1 (fr) * | 1977-10-17 | 1979-05-11 | Onera (Off Nat Aerospatiale) | Procede et installation pour le controle de l'efficacite des surfaces aerodynamiques d'un aeronef |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0680877A1 (fr) * | 1994-05-03 | 1995-11-08 | AEROSPATIALE Société Nationale Industrielle | Avion de transport à empennage avant |
| FR2719548A1 (fr) * | 1994-05-03 | 1995-11-10 | Aerospatiale | Avion de transport à empennage avant. |
| US5722615A (en) * | 1994-05-03 | 1998-03-03 | Aerospatiale Societe Nationale Indusrielle | Transport airplane with front empennage |
| EP0953504A1 (fr) | 1998-04-29 | 1999-11-03 | Aerospatiale Societe Nationale Industrielle | Aéronef à efforts de voilure diminués |
| FR2778163A1 (fr) | 1998-04-29 | 1999-11-05 | Aerospatiale | Aeronef a efforts de voilure diminues |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2043562A (en) | 1980-10-08 |
| DE2906889A1 (de) | 1980-09-04 |
| DE2906889C2 (de) | 1986-06-26 |
| FR2449592B1 (enrdf_load_stackoverflow) | 1984-11-23 |
| GB2043562B (en) | 1983-03-09 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB924022A (en) | Improvements relating to underwater vehicles | |
| FR2396947A1 (fr) | Surface de guidage aerodynamique a vecteur poussee integre | |
| GB1009269A (en) | Improvements in or relating to aircraft | |
| FR2449592A1 (fr) | Avion muni de surfaces de gouverne disposees devant et derriere le centre de gravite | |
| FR2438278A1 (fr) | Tete d'affichage pour collimateur de pilotage | |
| GB1014970A (en) | Improvements in and relating to the guiding of a remote controlled missile towards afreely movable target | |
| US2865579A (en) | Jet propulsion system for maintaining aircraft in a vertical attitude | |
| GB1204481A (en) | Improvements relating to take-off director systems for aircraft | |
| Kelley | Differential-turn maneuvering | |
| Malcolm et al. | Two specific kinds of disorientation incidents: Jet upset and giant hand(Contribution of reduced visibility and turbulence to loss of aircraft control and inadvertent aircraft maneuvers) | |
| BOGUSLAVSKII et al. | Control of a spacecraft with low-thrust engines during the boost phase in the absence of information on the instantaneous velocity vector(Low-thrust engine spacecraft control during boost phase, independent of velocity vector determination, by stabilizing osculating orbit plane relative to planetocentric coordinate system) | |
| Kelley | Differential-turn maneuvering | |
| FR2405869A1 (fr) | Procede et installation pour le controle de l'efficacite des surfaces aerodynamiques d'un aeronef | |
| FR71802E (fr) | Viseur universel sur avion (ou navire) pour la dérivométrie, l'atterrissage de précision, la conduite du pilotage, du bombardement en piqué par bombes ou fusées, du tir sur but au sol ou sur but aérien et du torpillage | |
| GOUARS | Psychophysiological impact of low-altitude high-speed flight in a high-performance single-seat aircraft(Pilot capability in low level high speed flying analyzed for influence of roughness fatigue, control improvements, vibration and visual problems) | |
| BABA et al. | Guidance law for a flight vehicle with constant acceleration | |
| GB1294851A (enrdf_load_stackoverflow) | ||
| KOENIG | Design optimization and testing of flight control systems for light helicopters(Design optimization and testing of flight control systems for light helicopters, applied to BO-105 helicopter) | |
| GB1227735A (enrdf_load_stackoverflow) | ||
| GB1284246A (en) | Means for the control of a jet propelled aircraft | |
| GB1388379A (en) | Aircraft | |
| Hammond | Optimal and suboptimal laws for simple homing systems | |
| GB1236372A (en) | Improvements in or relating to radio aerials for aircraft | |
| HACKER | Problem of optimum commands of a vertical- takeoff aircraft(Control laws providing attainment of prescribed attitude and acceleration to prescribed speed in minimum time or fuel consumption for VTOL AIRCRAFT) | |
| HOULT | The use of approximate analyses to determine the performance, authority, and impulse of sounding-rocket boost-control-systems(autopilot model for control of booster rocket engine) |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| CD | Change of name or company name | ||
| TP | Transmission of property | ||
| ST | Notification of lapse |