FR2436433A1 - Perfectionnements aux installations pour fournir une reference de roulis, notamment en vue du guidage d'engins - Google Patents
Perfectionnements aux installations pour fournir une reference de roulis, notamment en vue du guidage d'enginsInfo
- Publication number
- FR2436433A1 FR2436433A1 FR7826313A FR7826313A FR2436433A1 FR 2436433 A1 FR2436433 A1 FR 2436433A1 FR 7826313 A FR7826313 A FR 7826313A FR 7826313 A FR7826313 A FR 7826313A FR 2436433 A1 FR2436433 A1 FR 2436433A1
- Authority
- FR
- France
- Prior art keywords
- missile
- polarised
- laser diode
- directed onto
- provides
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/24—Beam riding guidance systems
- F41G7/26—Optical guidance systems
- F41G7/266—Optical guidance systems for spin-stabilized missiles
Abstract
Installation pour fournir une référence de roulis en vue du guidage d'un engin tournant sur sa trajectoire. L'installation comprend une station de commande comportant un émetteur de faisceau électromagnétique, notamment lumineux, polarisé rectilignement, vers l'engin 16. Elle comporte, de plus, un récepteur placé à bord de l'engin et comportant plusieurs ensembles détecteurs ayant chacun un capteur 18 de réception du faisceau à travers un analyseur et une électronique munie de moyens de lever de doute par évaluation du nombre de demi-tours de l'engin depuis son départ. Application au guidage d'un engin auto-propulsé tiré par effet canon.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7826313A FR2436433A1 (fr) | 1978-09-13 | 1978-09-13 | Perfectionnements aux installations pour fournir une reference de roulis, notamment en vue du guidage d'engins |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7826313A FR2436433A1 (fr) | 1978-09-13 | 1978-09-13 | Perfectionnements aux installations pour fournir une reference de roulis, notamment en vue du guidage d'engins |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2436433A1 true FR2436433A1 (fr) | 1980-04-11 |
FR2436433B1 FR2436433B1 (fr) | 1983-01-14 |
Family
ID=9212606
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7826313A Granted FR2436433A1 (fr) | 1978-09-13 | 1978-09-13 | Perfectionnements aux installations pour fournir une reference de roulis, notamment en vue du guidage d'engins |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2436433A1 (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0239156A1 (fr) * | 1986-03-20 | 1987-09-30 | Hollandse Signaalapparaten B.V. | Dispositif pour déterminer la position angulaire de roulis d'un objet animé d'un mouvement de rotation autour d'un axe |
US7589663B1 (en) * | 2006-01-20 | 2009-09-15 | The United States Of America As Represented By The Secretary Of The Army | System and method for the measurement of the unambiguous roll angle of a projectile |
US20130001354A1 (en) * | 2011-06-30 | 2013-01-03 | Northrop Grumman Guidance and Electronic Comany, Inc. | GPS independent guidance sensor system for gun-launched projectiles |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2116957A1 (de) * | 1971-04-07 | 1972-10-19 | Messerschmitt Boelkow Blohm | Optisches Lenksystem für sich selbsttätig bewegende Flugkörper |
FR2298821A1 (fr) * | 1975-01-27 | 1976-08-20 | Northrop Corp | Dispositif de reference de roulis pour vehicules commandes par faisceau optique |
US4072281A (en) * | 1976-12-27 | 1978-02-07 | The United States Of America As Represented By The Secretary Of The Army | Optical attitude reference |
-
1978
- 1978-09-13 FR FR7826313A patent/FR2436433A1/fr active Granted
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2116957A1 (de) * | 1971-04-07 | 1972-10-19 | Messerschmitt Boelkow Blohm | Optisches Lenksystem für sich selbsttätig bewegende Flugkörper |
FR2298821A1 (fr) * | 1975-01-27 | 1976-08-20 | Northrop Corp | Dispositif de reference de roulis pour vehicules commandes par faisceau optique |
US4072281A (en) * | 1976-12-27 | 1978-02-07 | The United States Of America As Represented By The Secretary Of The Army | Optical attitude reference |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0239156A1 (fr) * | 1986-03-20 | 1987-09-30 | Hollandse Signaalapparaten B.V. | Dispositif pour déterminer la position angulaire de roulis d'un objet animé d'un mouvement de rotation autour d'un axe |
US4750689A (en) * | 1986-03-20 | 1988-06-14 | Hollandse Signaalapparaten B.V. | System for determining the angular spin position of an object spinning about an axis |
US7589663B1 (en) * | 2006-01-20 | 2009-09-15 | The United States Of America As Represented By The Secretary Of The Army | System and method for the measurement of the unambiguous roll angle of a projectile |
US20130001354A1 (en) * | 2011-06-30 | 2013-01-03 | Northrop Grumman Guidance and Electronic Comany, Inc. | GPS independent guidance sensor system for gun-launched projectiles |
US8598501B2 (en) * | 2011-06-30 | 2013-12-03 | Northrop Grumman Guidance an Electronics Co., Inc. | GPS independent guidance sensor system for gun-launched projectiles |
Also Published As
Publication number | Publication date |
---|---|
FR2436433B1 (fr) | 1983-01-14 |
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